TWI622796B - Optical image capturing system - Google Patents

Abstract

An optical imaging system includes a first lens, a second lens, a third lens, and a fourth lens in this order from the object side to the image side. The first lens has a refractive power, and an object side surface thereof may be convex. The second lens to the third lens have a refractive power, and both surfaces of the foregoing lenses may be aspheric. The fourth lens may have a positive refractive power, and both surfaces thereof are aspherical, and at least one surface of the fourth lens may have a inflection point. The lenses with refractive power in the optical imaging system are the first lens to the fourth lens. When certain conditions are met, it can have greater light collection and better light path adjustment capabilities to improve imaging quality.

Description

Optical imaging system

The invention relates to an optical imaging system, and in particular to a miniaturized optical imaging system applied to electronic products.

In recent years, with the rise of portable electronic products with photographic functions, the demand for optical systems has been increasing. The photosensitive elements of general optical systems are nothing more than two types: photosensitive coupled devices (CCDs) or complementary metal-Oxide semiconduTPor sensors (CMOS sensors), and with the advancement of semiconductor process technology, The pixel size of the photosensitive element is reduced, and the optical system is gradually developed in the high pixel field, so the requirements for imaging quality are also increasing.

The optical systems traditionally mounted on portable devices mostly use two- or three-piece lens structures. However, as portable devices continue to improve pixel quality and end consumers ’demands for large apertures such as low light and night light The shooting function or the need for a wide viewing angle such as the self-timer function of the front lens. However, designing an optical system with a large aperture often faces the situation of generating more aberrations, which will cause the surrounding imaging quality to deteriorate and the difficulty of manufacturing, and designing a wide viewing angle optical system will face an increase in imaging distortion. Optical imaging systems have been unable to meet higher-level photographic requirements.

Therefore, how to effectively increase the amount of light entering the optical imaging system and increase the viewing angle of the optical imaging system, in addition to further improving the overall pixels and quality of the imaging, while taking into account the balanced design of the miniaturized optical imaging system, has become a very important issue.

The aspect of the embodiment of the present invention is directed to an optical imaging system that can use the combination of the refractive power of four lenses, a convex surface and a concave surface (the convex surface or concave surface of the present invention refers in principle to the object side or image side of each lens on the optical axis Geometric shape description above), which can effectively increase the amount of light entering the optical imaging system and increase the viewing angle of the optical imaging system, with a certain degree of contrast and Improve the total pixels and quality of imaging for small electronic products.

In addition, in specific optical imaging applications, there is a need to perform imaging for both light sources with visible and infrared wavelengths, such as IP video surveillance cameras. The "Day & Night" feature of IP video surveillance cameras is mainly because human visible light is located in the spectrum of 400-700nm, but the imaging of the sensor includes human invisible infrared light, so in order to ensure that The sensor finally retains only the visible light of the human eye. If necessary, a removable IR cut filter (ICR) is set in front of the lens to increase the "realism" of the image, which can eliminate infrared during the daytime. Light and avoid color shift; let infrared light come in at night to increase brightness. However, the ICR element itself occupies a considerable volume and is expensive, which is disadvantageous for the design and manufacture of future miniature surveillance cameras.

The aspect of the embodiment of the present invention is directed to an optical imaging system and an optical image capturing lens at the same time. The refractive power of the four lenses, the combination of convex and concave surfaces, and the selection of materials can be used to make the optical imaging system focus on visible light and infrared light. The gap between the imaging focal lengths is reduced, that is, it is close to the "confocal" effect, so there is no need to use ICR components.

The terms of the lens parameters related to the embodiments of the present invention and their codes are listed in detail as a reference for subsequent descriptions: lens parameters related to the magnification of the optical imaging system and the optical image capture lens

The optical imaging system and the optical image capturing lens of the present invention can also be designed for biometric identification, such as facial recognition. If the embodiment of the present invention is used for image capture of face recognition, infrared light may be used as the working wavelength. At the same time, for faces with a distance of about 25 to 30 cm and a width of about 15 cm, it can be applied to the photosensitive element (pixel size 1.4 micrometers (μm)) at least 30 horizontal pixels are imaged in the horizontal direction. The linear magnification of the infrared imaging surface is LM, which meets the following conditions: LM = (30 horizontal pixels) multiplied by (pixel size of 1.4 microns) divided by the width of the subject 15 cm; LM ≧ 0.0003. At the same time, visible light is used as the working wavelength. At the same time, at least 50 faces with a distance of about 25 to 30 cm and a width of about 15 cm can be imaged horizontally on a photosensitive element (pixel size is 1.4 micrometers (μm)). Horizontal pixels.

Lens parameters related to length or height

In the visible light spectrum, the present invention can select a wavelength of 555 nm as the main reference wavelength. As a benchmark for measuring focus shift, a wavelength of 850 nm can be selected as the main reference wavelength and a benchmark for measuring focus shift in the infrared light spectrum (700nm to 1000nm).

The optical imaging system has a first imaging plane and a second imaging plane. The first imaging plane is a visible light image plane perpendicular to the optical axis, and the central field of view is a defocus modulation conversion contrast transfer rate at a first spatial frequency. (MTF) has a maximum value; and the second imaging plane is a specific defocus modulation conversion contrast transfer ratio (MTF) of a specific infrared light image plane perpendicular to the optical axis and a central field of view at a first spatial frequency. The optical imaging system further has a first average imaging plane and a second average imaging plane. The first average imaging plane is a visible light image plane perpendicular to the optical axis and is set in the central field of view of the optical imaging system. The average position of the defocus position of the field and the 0.7 field of view each having the maximum MTF value of the field of view at the first spatial frequency; and the second average imaging plane is a specific infrared light image plane perpendicular to the optical axis and is set at The central field of view, the 0.3 field of view, and the 0.7 field of view of the optical imaging system each have an average position of an out-of-focus position having a maximum MTF value of each of the fields at a first spatial frequency.

The aforementioned first spatial frequency is set to a half of the spatial frequency (half frequency) of the photosensitive element (sensor) used in the present invention. For example, the pixel size is a photosensitive element containing 1.12 micrometers or less, and its modulation conversion function characteristic is The quarter space frequency, half space frequency (half frequency) and full space frequency (full frequency) of the figure are at least 110 cycles / mm, 220 cycles / mm, and 440 cycles / mm, respectively. The light in any field of view can be further divided into sagittal ray and tangential ray.

The focus offset of the maximum defocus MTF of the sagittal rays of the visible light center field of view, 0.3 field of view, and 0.7 field of view of the optical imaging system of the present invention is represented by VSFS0, VSFS3, and VSFS7 (unit of measurement: mm); The maximum defocus MTF of the sagittal plane rays of the field of view, 0.3 field of view, and 0.7 field of view are represented by VSMTF0, VSMTF3, and VSMTF7, respectively; the maximum defocus MTF of the meridional rays of the central field of view, 0.3 field of view, and 0.7 field of view The value of the focus offset is represented by VTFS0, VTFS3, and VTFS7 (measurement unit: mm); the maximum defocus MTF of the meridional rays of the central field of view, 0.3 field of view, and 0.7 field of view is VTMTF0, VTMTF3, and VTMTF7, respectively. Means. The average focus shift amount (position) of the focus shift amounts of the aforementioned sagittal three-view field of the visible arc and the meridional three-view field of visible light is represented by AVFS (measurement unit: mm), which satisfies the absolute value | (VSFS0 + VSFS3 + VSFS7 + VTFS0 + VTFS3 + VTFS7) / 6 ｜.

The focus offset of the maximum defocus MTF of the sagittal plane rays of the central field, the 0.3 field of view, and the 0.7 field of vision of the optical imaging system of the present invention is represented by ISFS0, ISFS3, and ISFS7, respectively. The average focus offset (position) of the focus offset is expressed in AISFS (measurement unit: mm); the maximum defocus MTF of the sagittal rays of the infrared central field, 0.3 field of view, and 0.7 field of view is ISMTF0, ISMTF3 and ISMTF7 are indicated; the focus offset of the maximum defocus MTF of the meridional rays of the central field of view, 0.3 field of view, and 0.7 field of view of the infrared light is represented by ITFS0, ITFS3, and ITFS7 (unit of measurement: mm), the aforementioned meridian The average focus offset (position) of the focus offset of the three fields of view is expressed by AITFS (unit of measurement: mm); the center of field of infrared light, 0.3 field of view, and 0.7 field of view have the largest defocus MTF of the meridional rays The values are expressed as IMTTF0, IMTTF3, and IMTTF7, respectively. The average focus offset (position) of the aforementioned infrared light sagittal three-field and infrared light meridional three-field is represented by AIFS (unit of measurement: mm), which satisfies the absolute value | (ISFS0 + ISFS3 + ISFS7 + ITFS0 + ITFS3 + ITFS7) / 6 ｜.

The focus offset between the visible light center field focus point and the infrared light center field focus point (RGB / IR) of the entire optical imaging system is represented by FS (ie, wavelength 850nm vs. wavelength 555nm, unit of measurement: mm), which satisfies Absolute value ｜ (VSFS0 + VTFS0) / 2- (ISFS0 + ITFS0) / 2 ｜; The average focus shift of visible light three-view field and the average focus shift of three-field infrared light (RGB / IR) The difference between them (focus shift amount) is expressed in AFS (that is, a wavelength of 850 nm to a wavelength of 555 nm, a unit of measurement: mm), which satisfies the absolute value | AIFS-AVFS |.

The maximum imaging height of the optical imaging system is represented by HOI; the height of the optical imaging system is represented by HOS; the distance between the first lens object side and the fourth lens image side of the optical imaging system is represented by InTL; the fourth lens image of the optical imaging system The distance from the side to the imaging surface is represented by InB; InTL + InB = HOS; the distance from the fixed light barrier (aperture) of the optical imaging system to the imaging surface is represented by InS; the distance between the first lens and the second lens of the optical imaging system The distance is represented by IN12 (example); the thickness of the first lens of the optical imaging system on the optical axis is represented by TP1 (example).

Lens parameters related to materials

The dispersion coefficient of the first lens of the optical imaging system is represented by NA1 (illustration); the refraction law of the first lens is represented by Nd1 (illustration).

Angle-dependent lens parameters

The angle of view is represented by AF; half of the angle of view is represented by HAF; the principal ray angle is represented by MRA.

Lens parameters related to exit pupil

The entrance pupil diameter of the optical imaging system is represented by HEP; the exit pupil of the optical imaging system refers to the image formed by the aperture diaphragm passing through the lens group behind the aperture diaphragm in the image space, and the exit pupil diameter is represented by HPP; single lens The maximum effective radius of any surface refers to the intersection point (Effective Half Diameter; EHD) at the lens surface at the maximum viewing angle of incident light passing through the edge of the entrance pupil, and the vertical height between the intersection point and the optical axis. For example, the maximum effective radius of the object side of the first lens is represented by EHD11, and the maximum effective radius of the image side of the first lens is represented by EHD12. The maximum effective radius of the object side of the second lens is represented by EHD21, and the maximum effective radius of the image side of the second lens is represented by EHD22. The maximum effective radius of any surface of the remaining lenses in the optical imaging system is expressed in the same manner.

Parameters related to lens surface arc length and surface contour

The length of the contour curve of the maximum effective radius of any surface of a single lens refers to the starting point of the intersection of the surface of the lens and the optical axis of the optical imaging system to which it belongs, from the starting point along the surface contour of the lens to its Up to the end of the maximum effective radius, the arc length of the curve between the two points is the length of the contour curve of the maximum effective radius, and it is expressed by ARS. For example, the length of the contour curve of the maximum effective radius on the object side of the first lens is represented by ARS11, and the length of the contour curve of the maximum effective radius of the image side of the first lens is represented by ARS12. The length of the contour curve of the maximum effective radius on the object side of the second lens is represented by ARS21, and the length of the contour curve of the maximum effective radius of the image side of the second lens is represented by ARS22. The length of the contour curve of the maximum effective radius of any surface of the remaining lenses in the optical imaging system is expressed in the same manner.

The length of the contour curve of 1/2 of the entrance pupil diameter (HEP) of any surface of a single lens refers to the intersection of the surface of the lens and the optical axis of the optical imaging system to which it belongs as the starting point. The surface contour of the lens is up to the coordinate point of the vertical height of 1/2 of the entrance pupil diameter from the optical axis on the surface. The curve arc length between the two points is 1/2 the length of the contour curve of the entrance pupil diameter (HEP). ARE said. For example, the contour curve length of 1/2 incident pupil diameter (HEP) on the object side of the first lens is represented by ARE11, and the contour curve length of 1/2 incident pupil diameter (HEP) on the image side of the first lens is represented by ARE12. The length of the profile curve of 1/2 incident pupil diameter (HEP) on the object side of the second lens is represented by ARE21, and the length of the profile curve of 1/2 incident pupil diameter (HEP) on the image side of the second lens is represented by ARE22. 1/2 of any surface of the remaining lenses in the optical imaging system The contour curve length of the entrance pupil diameter (HEP) is expressed in the same manner.

Parameters related to lens surface depth

The horizontal displacement distance of the intersection of the fourth lens object side on the optical axis to the maximum effective radius position of the fourth lens object side on the optical axis is represented by InRS41 (illustration); the fourth lens image side intersection on the optical axis to the fourth The horizontal displacement distance of the maximum effective radius position of the lens image side on the optical axis is represented by InRS42 (example).

Parameters related to lens shape

The critical point C refers to a point on a specific lens surface that is tangent to a tangent plane that is perpendicular to the optical axis except for the intersection with the optical axis. For example, the vertical distance between the critical point C31 on the object side of the third lens and the optical axis is HVT31 (example), and the vertical distance between the critical point C32 on the image side of the third lens and the optical axis is HVT32 (example). The fourth lens object The vertical distance between the critical point C41 on the side and the optical axis is HVT41 (illustrated), and the vertical distance between the critical point C42 on the fourth lens image side and the optical axis is HVT42 (illustrated). The critical points on the object side or image side of other lenses and their vertical distance from the optical axis are expressed in the same manner as described above.

The inflection point closest to the optical axis on the object side of the fourth lens is IF411, and the point subsidence SGI411 (for example), SGI411 is the intersection of the object side of the fourth lens on the optical axis to the closest optical axis of the object side of the fourth lens. The horizontal displacement distance between the inflection points parallel to the optical axis. The vertical distance between this point and the optical axis of IF411 is HIF411 (illustration). The inflection point on the image side of the fourth lens closest to the optical axis is IF421. This point has a subsidence of SGI421 (example). SGI411 is the intersection of the fourth lens image side on the optical axis to the closest optical axis of the fourth lens image side. The horizontal displacement distance between the inflection points is parallel to the optical axis. The vertical distance between this point and the optical axis is IF421 (illustration).

The second inflection point on the object side of the fourth lens that is close to the optical axis is IF412. This point has a subsidence of SGI412 (example). SGI412 is the intersection of the object side of the fourth lens on the optical axis and the second object is close to the fourth lens object side. The horizontal displacement distance between the inflection points of the optical axis is parallel to the optical axis, and the vertical distance between this point of IF412 and the optical axis is HIF412 (illustration). The second inflection point on the fourth lens image side that is close to the optical axis is IF422. This point sinks SGI422 (for example). SGI422 is the intersection of the fourth lens image side on the optical axis to the fourth lens image side. The horizontal displacement distance between the inflection points of the optical axis is parallel to the optical axis, and the vertical distance between this point of the IF422 and the optical axis is HIF422 (example).

The third inflection point on the object side of the fourth lens that is close to the optical axis is IF413. This point has a subsidence of SGI413 (example). SGI413 is the intersection of the object side of the fourth lens on the optical axis to the fourth lens. The horizontal displacement distance parallel to the optical axis between the third inflection point on the side of the lens and the optical axis is parallel, and the vertical distance between this point and the optical axis of IF4132 is HIF413 (illustration). The third inflection point on the fourth lens image side close to the optical axis is IF423. This point has a subsidence of SGI423 (example). SGI423, that is, the intersection of the fourth lens image side on the optical axis and the fourth lens image side third approach. The horizontal displacement distance between the inflection points of the optical axis is parallel to the optical axis. The vertical distance between this point and the optical axis of IF423 is HIF423 (illustration).

The inflection point on the fourth lens object side close to the optical axis is IF414. This point has a subsidence of SGI414 (example). SGI414 is the intersection of the fourth lens object side on the optical axis to the fourth lens object side. The horizontal displacement distance between the inflection points of the optical axis is parallel to the optical axis, and the vertical distance between this point of IF414 and the optical axis is HIF414 (illustration). The inflection point on the fourth lens image side close to the optical axis is IF424, and the point subsidence SGI424 (example), SGI424, that is, the intersection of the fourth lens image side on the optical axis to the fourth lens image side fourth approach The horizontal displacement distance between the inflection points of the optical axis is parallel to the optical axis, and the vertical distance between this point and the optical axis of IF424 is HIF424 (illustration).

The inflection points on the object side or image side of other lenses and their vertical distance from the optical axis or the amount of their subsidence are expressed in the same manner as described above.

Aberration-related variables

Optical Distortion of an optical imaging system is represented by ODT; its TV Distortion is represented by TDT, and the degree of aberration shift between 50% and 100% of the field of view can be further defined; spherical aberration bias The amount of shift is expressed in DFS; the amount of comet aberration shift is expressed in DFC.

The lateral aberration of the aperture edge is expressed by STA (STOP Transverse Aberration). To evaluate the performance of a specific optical imaging system, you can use a tangential fan or a sagittal fan to calculate the horizontal direction of any field of view. Aberrations, in particular, the lateral aberrations of the longest operating wavelength (for example, a wavelength of 650NM) and the shortest operating wavelength (for example, a wavelength of 470NM) passing through the aperture edge are used as standards for excellent performance. The coordinate directions of the aforementioned meridional light fans can be further divided into positive (upper light) and negative (lower light) directions. The lateral aberration of the longest working wavelength passing through the aperture edge is defined as the imaging position where the longest working wavelength is incident on the imaging surface through the edge of the aperture, and it is on the imaging surface with the main wavelength of the reference wavelength (for example, 555NM). The distance between the two positions of the imaging position of the field. The shortest working wavelength passes through the lateral aberration of the aperture edge. It is defined as the imaging position where the shortest working wavelength is incident on the imaging plane through the edge of the aperture. The distance difference between the two positions of the imaging position of the field of view on the imaging surface. The performance of the specific optical imaging system is excellent. The shortest and longest working wavelengths can be used to enter the imaging surface through the edge of the aperture and the 0.7 field of view (that is, 0.7 imaging height HOI) is less than 50 microns (μm) as the inspection method. It is even possible to further use the shortest and longest working wavelengths incident on the imaging surface through the edge of the aperture as the 0.7 field of view with lateral aberrations less than 30 micrometers (μm) as the inspection method.

The optical imaging system has a maximum imaging height HOI perpendicular to the optical axis on the imaging plane. The longest working wavelength of the positive meridional fan of the optical imaging system passes through the edge of the entrance pupil and is incident on a lateral image at 0.7 HOI on the imaging plane. The difference is represented by PLTA. The shortest working wavelength of the positive meridional fan passes through the edge of the entrance pupil and is incident on the imaging plane at 0.7HOI. The lateral aberration is represented by PSTA. The longest working wavelength of the negative meridional fan passes. The lateral aberration of the entrance pupil edge and incident on the imaging plane at 0.7HOI is expressed by NLTA. The shortest working wavelength of the negative meridional fan passes through the entrance pupil edge and is incident on the imaging plane at 0.7HOI. The difference is represented by NSTA. The longest working wavelength of the sagittal plane fan passes through the edge of the entrance pupil and is incident on the imaging plane at 0.7HOI. The lateral aberration is represented by SLTA. The shortest operating wavelength of the sagittal plane fan passes through the edge of the entrance pupil. The lateral aberration at 0.7 HOI incident on the imaging plane is represented by SSTA.

The present invention provides an optical imaging system, in which the object side or the image side of the fourth lens is provided with inflection points, which can effectively adjust the angle of each field of view incident on the fourth lens, and correct optical distortion and TV distortion. In addition, the surface of the fourth lens may have better light path adjustment capabilities to improve imaging quality.

According to the present invention, an optical imaging system is provided, which includes a first lens, a second lens, a third lens, a fourth lens, a first imaging surface, and a second imaging surface in order from the object side to the image side. The first imaging plane is a specific visible light image plane perpendicular to the optical axis, and the central field of view has a maximum defocus modulation conversion contrast transfer rate (MTF) at the first spatial frequency; the second imaging plane is a specific vertical The defocus modulation conversion contrast transfer rate (MTF) of the infrared light image plane at the optical axis and its central field of view at the first spatial frequency has a maximum value. Each of the first to fourth lenses has a refractive power. The focal lengths of the first lens to the fourth lens are f1, f2, f3, and f4, the focal length of the optical imaging system is f, the entrance pupil diameter of the optical imaging system is HEP, and the object side of the first lens is connected to the first lens. An imaging plane has a distance HOS on the optical axis, half of the maximum viewing angle of the optical imaging system is HAF, the optical imaging system has a maximum imaging height HOI perpendicular to the optical axis on the first imaging plane, and the first The distance between the imaging plane and the second imaging plane on the optical axis is FS, and the red The wavelength of external light is between 700nm and 1000nm and the first spatial frequency is represented by SP1. The intersection of any surface of any of these lenses with the optical axis is the starting point, and extends the contour of the surface until the distance from the surface to the light. Up to the coordinate point at the vertical height of the axis 1/2 incident pupil diameter, the length of the contour curve between the two points is ARE, which meets the following conditions: 1 ≦ f / HEP ≦ 10; 0deg <HAF ≦ 70deg; SP1 ≦ 440cycles / mm; 1 ≦ 2 (ARE / HEP) ≦ 2.0; and | FS | ≦ 30 μm.

According to the present invention, there is provided an optical imaging system, which includes a first lens, a second lens, a third lens, a fourth lens, a first imaging surface, and a second imaging surface in order from the object side to the image side. The first imaging plane is a specific visible light image plane perpendicular to the optical axis, and the central field of view has a maximum defocus modulation conversion contrast transfer rate (MTF) at the first spatial frequency; the second imaging plane is a specific vertical The defocus modulation conversion contrast transfer rate (MTF) of the infrared light image plane at the optical axis and its central field of view at the first spatial frequency has a maximum value. The first lens has a positive refractive power. The second lens has a refractive power and its image side is convex on the optical axis; the third lens has a refractive power and its image side is convex on the optical axis. The focal lengths of the first lens to the fourth lens are f1, f2, f3, and f4, the focal length of the optical imaging system is f, the entrance pupil diameter of the optical imaging system is HEP, and the object side of the first lens is connected to the first lens. An imaging plane has a distance HOS on the optical axis, half of the maximum viewing angle of the optical imaging system is HAF, the optical imaging system has a maximum imaging height HOI perpendicular to the optical axis on the first imaging plane, and the first The distance between the imaging surface and the second imaging surface on the optical axis is FS. The intersection of any surface of any of the lenses with the optical axis is the starting point, and extends the contour of the surface until the surface is away from the optical axis. Up to the coordinate point at the vertical height of 1/2 of the entrance pupil diameter, the length of the contour curve between the two points is ARE, which meets the following conditions: 1 ≦ f / HEP ≦ 10; 0deg <HAF ≦ 70deg; 1 ≦ 2 (ARE /HEP)≦2.0 and | FS | ≦ 30 μm.

According to the present invention, there is further provided an optical imaging system, which includes a first lens, a second lens, a third lens, a fourth lens, a first average imaging surface, and a second average imaging surface in this order from the object side to the image side. The first average imaging plane is a visible light image plane perpendicular to the optical axis and is arranged in the central field of view, the field of view of 0.3, and the field of view of 0.7 of the optical imaging system. Each of the first spatial frequencies has a maximum MTF of the field of view. The average position of the defocus position of the value; the second average imaging plane is a specific infrared light image plane perpendicular to the optical axis and is set in the central field of view, 0.3 field of view, and 0.7 field of view of the optical imaging system. The spatial frequencies all have an average position of the out-of-focus position of the maximum MTF value of the field of view. The first lens has a positive refractive power. The second lens has a refractive power And its image side is convex on the optical axis; the third lens has a positive refractive power and its image side is convex on the optical axis. The focal lengths of the first lens to the fourth lens are f1, f2, f3, and f4, the focal length of the optical imaging system is f, the entrance pupil diameter of the optical imaging system is HEP, and the object side of the first lens is connected to the first lens. An average imaging plane has a distance HOS on the optical axis, half of the maximum viewing angle of the optical imaging system is HAF, and the optical imaging system has a maximum imaging height HOI perpendicular to the optical axis on the first average imaging plane. The intersection of any surface of any of these lenses with the optical axis is the starting point, and extends the contour of the surface until the coordinate point on the surface at a vertical height of 1/2 of the entrance pupil diameter of the optical axis. The length of the contour curve is ARE, the distance between the first average imaging plane and the second average imaging plane is AFS, and the distance between the first average imaging plane and the second average imaging plane on the optical axis is FS, which satisfies The following conditions: 1 ≦ f / HEP ≦ 10; 0deg <HAF ≦ 70deg; 1 ≦ 2 (ARE / HEP) ≦ 2.0 and | AFS | ≦ 30 μm.

One half of the maximum vertical viewing angle of the optical imaging system is VHAF, and the optical imaging system satisfies the following formula: VHAF ≧ 10deg.

The optical imaging system satisfies the following conditions: HOS / HOI ≧ 1.2.

The intersection of the object-side surface of the fourth lens on the optical axis is the starting point, and extends the contour of the surface until the coordinate point on the surface at a vertical height of 1/2 of the entrance pupil diameter from the optical axis. The length of the contour curve is ARE41. The intersection of the image-side surface of the fourth lens on the optical axis is the starting point, and the contour of the surface is extended to the coordinate point on the surface at a vertical height of 1/2 of the entrance pupil diameter from the optical axis. So far, the length of the contour curve between the two points is ARE42, and the thickness of the fourth lens on the optical axis is TP4, which satisfies the following conditions: 0.05 ≦ ARE41 / TP4 ≦ 25; and 0.05 ≦ ARE42 / TP4 ≦ 25.

The first lens has a negative refractive power. The TV distortion of the optical imaging system at the time of image formation is TDT, and the longest working wavelength of the positive meridional fan of the optical imaging system passes through the edge of the entrance pupil and enters the lateral aberration at 0.7HOI on the imaging plane. PLTA indicates that the shortest working wavelength of the positive meridional fan passes through the edge of the entrance pupil and is incident on the imaging surface at 0.7HOI. The lateral aberration is represented by PSTA, and the longest working wavelength of the negative meridional fan passes through the incident. Lateral aberration at the edge of the pupil and incident on this imaging plane at 0.7HOI Expressed in NLTA, the shortest working wavelength of the negative meridional fan passes through the edge of the entrance pupil and the transverse aberration at 0.7HOI incident on the imaging plane is represented by NSTA. The longest working wavelength of the sagittal plane fan passes through the entrance pupil edge The lateral aberration at 0.7HOI incident on the imaging plane is represented by SLTA. The shortest working wavelength of the sagittal plane fan passes through the edge of the entrance pupil and incident at 0.7HOI on the imaging plane is represented by SSTA. The following conditions are satisfied: PLTA ≦ 100 microns; PSTA ≦ 100 microns; NLTA ≦ 100 microns; NSTA ≦ 100 microns; SLTA ≦ 100 microns; and SSTA ≦ 100 microns; | TDT | <100%.

The maximum effective radius of any surface of any of the lenses is represented by EHD. The intersection of any surface of any of the lenses of the lenses with the optical axis is the starting point, and extends the contour of the surface to the maximum of the surface. The effective radius is the end point. The length of the contour curve between the two points is ARS, which satisfies the following formula: 1 ≦ ARS / EHD ≦ 2.0.

One half of the maximum vertical viewing angle of the optical imaging system is VHAF, and the optical imaging system satisfies the following formula: VHAF ≧ 20deg.

The optical imaging system satisfies the following conditions: HOS / HOI ≧ 1.4.

The distance between the first lens and the second lens on the optical axis is IN12, and the following formula is satisfied: 0 <IN12 / f ≦ 60.

The distance between the third lens and the fourth lens on the optical axis is IN34, and the thicknesses of the third lens and the fourth lens on the optical axis are TP3 and TP4, which meet the following conditions: 1 ≦ (TP4 + IN34) / TP3 ≦ 10.

The optical imaging system meets the following conditions: HOS / HOI ≧ 1.6.

The length of the contour curve of any surface of a single lens within the maximum effective radius affects the surface's ability to correct aberrations and the optical path difference between rays of each field of view. The longer the length of the contour curve, the greater the ability to correct aberrations. It will increase the difficulty in production. Therefore, it is necessary to control the length of the contour curve within the maximum effective radius of any surface of a single lens, especially the length of the contour curve (ARS) and the surface within the maximum effective radius of the surface. All It belongs to the proportional relationship (ARS / TP) between the thickness (TP) of the lens on the optical axis. For example, the length of the contour curve of the maximum effective radius on the object side of the first lens is represented by ARS11, the thickness of the first lens on the optical axis is TP1, and the ratio between the two is ARS11 / TP1. The length of the contour curve is represented by ARS12, and the ratio between it and TP1 is ARS12 / TP1. The length of the contour curve of the maximum effective radius on the object side of the second lens is represented by ARS21, the thickness of the second lens on the optical axis is TP2, and the ratio between the two is ARS21 / TP2. The contour of the maximum effective radius of the image side of the second lens The length of the curve is represented by ARS22, and the ratio between it and TP2 is ARS22 / TP2. The proportional relationship between the length of the contour curve of the maximum effective radius of any of the surfaces of the remaining lenses in the optical imaging system and the thickness (TP) of the lens on the optical axis to which the surface belongs, and the expressions are deduced by analogy.

The length of the contour curve of any surface of a single lens within the height range of 1/2 entrance pupil diameter (HEP) particularly affects the ability of the surface to correct aberrations in the common area of each ray field of view and the optical path difference between the fields of light. The longer the length of the contour curve, the better the ability to correct aberrations. However, it will also increase the difficulty of manufacturing. Therefore, it is necessary to control the contour of any surface of a single lens within the height of 1/2 incident pupil diameter (HEP) The length of the curve, especially the proportional relationship between the length of the contour curve (ARE) within the height of 1/2 of the entrance pupil diameter (HEP) of the surface and the thickness (TP) of the lens on the optical axis to which the surface belongs (ARE / TP). For example, the length of the contour curve of the 1/2 entrance pupil diameter (HEP) height of the side of the first lens is represented by ARE11, the thickness of the first lens on the optical axis is TP1, and the ratio between the two is ARE11 / TP1. The length of the profile curve of the 1/2 entrance pupil diameter (HEP) height on the side of the mirror is represented by ARE12, and the ratio between it and TP1 is ARE12 / TP1. The length of the profile curve of the 1/2 entrance pupil diameter (HEP) height of the second lens object side is represented by ARE21, the thickness of the second lens on the optical axis is TP2, and the ratio between the two is ARE21 / TP2. The second lens image The profile curve length of the 1/2 entrance pupil diameter (HEP) height on the side is represented by ARE22, and the ratio between it and TP2 is ARE22 / TP2. The proportional relationship between the length of the contour curve of 1/2 of the entrance pupil diameter (HEP) height of any of the surfaces of the remaining lenses in the optical imaging system and the thickness (TP) of the lens on the optical axis to which the surface belongs. And so on.

The foregoing optical imaging system can be used with an image sensing element having a diagonal length of 1 / 1.2 inches or less. The size of the image sensing element is preferably 1 / 2.3 inches. The pixel size is less than 1.4 micrometers (μm), preferably the pixel size is less than 1.12 micrometers (μm), and the best pixel size is less than 0.9 micrometers (μm). In addition, the optical imaging system can Suitable for image sensing elements with an aspect ratio of 16: 9.

The aforementioned optical imaging system is applicable to the video recording requirements of more than one million or ten million pixels (for example, 4K2K or UHD, QHD) and has good imaging quality.

When | f1 |> f4, the total height of the optical imaging system (HOS; Height of Optic System) can be appropriately shortened to achieve the purpose of miniaturization.

When | f2 | + | f3 |> | f1 | + | f4 |, at least one of the lenses from the second lens to the third lens has a weak positive refractive power or a weak negative refractive power. The so-called weak refractive power means that the absolute value of the focal length of a particular lens is greater than 10. When at least one of the second lens to the third lens of the present invention has a weak positive refractive power, it can effectively share the positive refractive power of the first lens and prevent unnecessary aberrations from appearing prematurely. If at least one of the three lenses has a weak negative refractive power, the aberration of the correction system can be fine-tuned.

The fourth lens may have a positive refractive power. In addition, at least one surface of the fourth lens may have at least one inflection point, which can effectively suppress the angle of incidence of the off-axis field of view light, and further correct the aberration of the off-axis field of view.

1, 20, 30, 40, 50, 60‧‧‧ optical imaging system

100, 200, 300, 400, 500, 600‧‧‧ aperture

110, 210, 310, 410, 510, 610‧‧‧ first lens

112, 212, 312, 412, 512, 612

114, 214, 314, 414, 514, 614‧‧‧ like side

120, 220, 320, 420, 520, 620‧‧‧ second lens

122, 222, 322, 422, 522, 622

124, 224, 324, 424, 524, 624‧‧‧ like side

130, 230, 330, 430, 530, 630‧‧‧ third lens

132, 232, 332, 432, 532, 632

134, 234, 334, 434, 534, 634 ‧ ‧ like side

140, 240, 340, 440, 540, 640‧‧‧ fourth lens

142, 242, 342, 442, 542, 642

144, 244, 344, 444, 544, 644‧‧‧ like side

170, 270, 370, 470, 570, 670‧‧‧ infrared filters

180, 280, 380, 480, 580, 680‧‧‧ imaging surface

190, 290, 390, 490, 590, 690‧‧‧ image sensor

f‧‧‧ focal length of optical imaging system

f1‧‧‧ focal length of the first lens

f2‧‧‧ focal length of the second lens

f3‧‧‧ focal length of the third lens

f4‧‧‧ focal length of the fourth lens

f / HEP; Fno; F # ‧‧‧ aperture value of optical imaging system

HAF‧‧‧half of the maximum viewing angle of optical imaging system

NA1‧‧‧The dispersion coefficient of the first lens

NA2, NA3, NA4‧‧‧The dispersion coefficient of the second lens to the fourth lens

R1, R2‧The curvature radius of the object side and the image side of the first lens

R3, R4‧The curvature radius of the object side and the image side of the second lens

R5, R6‧The curvature radius of the object side and image side of the third lens

R7, R8‧The curvature radius of the object side and image side of the fourth lens

TP1‧‧‧thickness of the first lens on the optical axis

TP2, TP3, TP4‧thickness of the second to fourth lens on the optical axis

ΣTP‧‧‧ Total thickness of all refractive lenses

IN12‧‧‧ The distance between the first lens and the second lens on the optical axis

IN23‧‧‧ The distance between the second lens and the third lens on the optical axis

IN34‧‧‧ The distance between the third lens and the fourth lens on the optical axis

InRS41‧The horizontal displacement distance from the intersection of the fourth lens object side on the optical axis to the maximum effective radius position of the fourth lens object side on the optical axis

IF411‧‧‧the inflection point closest to the optical axis on the object side of the fourth lens

SGI411‧‧‧The amount of subsidence at this point

HIF411‧‧‧ The vertical distance between the inflection point closest to the optical axis on the object side of the fourth lens and the optical axis

IF421‧‧‧The closest inflection point on the image side of the fourth lens closest to the optical axis

SGI421‧‧‧ Subsidence

HIF421‧The vertical distance between the inflection point of the fourth lens image closest to the optical axis and the optical axis

IF412‧‧‧The second inflection point on the object side of the fourth lens near the optical axis

SGI412‧‧‧ Subsidence

HIF412‧The vertical distance between the second curved point near the optical axis on the object side of the fourth lens and the optical axis

IF422‧‧‧The second inflection point on the image side of the fourth lens close to the optical axis

SGI422‧‧‧The amount of subsidence at this point

HIF422‧‧‧ The vertical distance between the second curved point near the optical axis of the fourth lens image side and the optical axis

IF413‧‧‧The third inflection point on the object side of the fourth lens near the optical axis

SGI413‧‧‧The amount of subsidence at this point

HIF413‧‧‧ The vertical distance between the inflection point of the third lens object near the optical axis and the optical axis

IF423‧‧‧ the third inflection point close to the optical axis on the side of the fourth lens image

SGI423‧‧‧; subsidence at this point

HIF423 ‧‧‧ The vertical distance between the third lens near the inflection point on the image side and the optical axis

IF414‧‧‧The fourth inflection point on the object side of the fourth lens near the optical axis

SGI414‧‧‧The amount of subsidence at this point

HIF414‧‧‧ The vertical distance between the fourth curved lens near the optical axis and the optical axis

IF424‧‧‧ the fourth inflection point on the image side of the fourth lens close to the optical axis

SGI424‧‧‧The amount of subsidence at this point

HIF424‧‧‧ The vertical distance between the fourth lens image side and the fourth point close to the optical axis and the optical axis

C41‧‧‧ critical point of the object side of the fourth lens

C42‧ critical point of the image side of the fourth lens

SGC41‧‧‧Horizontal displacement distance between the critical point of the object side of the fourth lens and the optical axis

SGC42‧Horizontal displacement distance between the critical point of the image side of the fourth lens and the optical axis

HVT41‧‧‧ The vertical distance between the critical point of the object side of the fourth lens and the optical axis

HVT42‧‧‧ The vertical distance between the critical point of the image side of the fourth lens and the optical axis

HOS‧‧‧ total system height (distance from the first lens object side to the imaging plane on the optical axis)

Dg‧‧‧ diagonal length of image sensing element

InS‧‧‧ distance from aperture to imaging surface

InTL‧‧‧The distance from the object side of the first lens to the image side of the fourth lens

InB‧‧‧The distance from the image side of the fourth lens to the imaging surface

HOI‧‧‧ half of the diagonal length of the effective sensing area of the image sensing element (maximum image height)

TDT‧‧‧TV Distortion of Optical Imaging System

ODT‧‧‧Optical Distortion of Optical Imaging System

The above and other features of the present invention will be described in detail with reference to the drawings.

FIG. 1A is a schematic diagram showing the optical imaging system of the first embodiment of the present invention; FIG. 1B is a diagram showing the spherical aberration, astigmatism, and optical distortion of the optical imaging system of the first embodiment of the present invention in order from left to right. Graph; FIG. 1C is a transverse aberration diagram of a meridional fan and a sagittal fan of the optical imaging system according to the first embodiment of the present invention, the longest working wavelength and the shortest working wavelength passing through the edge of the aperture at a field of view of 0.7; FIG. 1D is a diagram showing the center field of view, 0.3 field of view, and 0.7 field of view of the visible light spectrum in accordance with the first embodiment of the present invention. FIG. The central field of view, the field of view of 0.3, and the field of view of 0.7 of the first embodiment of the infrared light spectrum are compared with the transfer rate diagram; FIG. 2A is a schematic diagram showing an optical imaging system according to the second embodiment of the present invention; Figure 2B shows the spherical aberration, astigmatism, and optical distortion of the optical imaging system according to the second embodiment of the present invention in order from left to right. Figure 2C shows the optical imaging system of the second embodiment of the present invention. Radial aberration light fan and sagittal light fan, the longest working wavelength and the shortest working wavelength are transverse aberration diagrams at the 0.7 field of view through the edge of the aperture; the 2D diagram is the central field of view of the visible light spectrum of the second embodiment of the present invention , 0.3 field of view, 0.7 field of view defocus modulation conversion contrast transfer rate chart; Figure 2E shows the central field of view, 0.3 field of view, 0.7 field of view of the infrared light spectrum of the second embodiment of the present invention Conversion contrast transfer rate diagram; FIG. 3A is a schematic diagram showing an optical imaging system according to a third embodiment of the present invention; FIG. 3B is a diagram showing the spherical aberration, Graph of astigmatism and optical distortion; Figure 3C shows the meridional fan and sagittal fan of the third embodiment of the optical imaging system of the present invention. The longest working wavelength and the shortest working wavelength pass through the edge of the aperture at a field of view of 0.7. Horizontal image FIG. 3D is a diagram showing the defocus modulation conversion contrast transfer rate of the central field of view, 0.3 field of view, and 0.7 field of view of the visible light spectrum of the third embodiment of the present invention; FIG. 3E is a view showing the third embodiment of the present invention Example of the central field of view, 0.3 field of view, 0.7 field of view of the infrared light spectrum of the defocus modulation conversion contrast transfer rate chart; Figure 4A is a schematic diagram showing an optical imaging system of a fourth embodiment of the present invention; Figure 4B is From left to right, the graphs of spherical aberration, astigmatism, and optical distortion of the optical imaging system of the fourth embodiment of the present invention are sequentially plotted; FIG. 4C is a meridional light fan of the optical imaging system of the fourth embodiment of the present invention. And sagittal plane fan, the longest working wavelength and the shortest working wavelength pass through the edge of the aperture at a 0.7 field of view. Lateral aberration diagram; FIG. 4D is a diagram showing the central field of view, 0.3 field of view, and 0.7 field of view of the visible spectrum of the fourth embodiment of the present invention with defocus modulation conversion contrast transfer rate; FIG. 4E is a diagram illustrating the present invention The central field of view, the field of view of 0.3, and the field of view of 0.7 in the fourth embodiment are compared with the defocus modulation conversion contrast transfer rate diagram; FIG. 5A is a schematic diagram showing an optical imaging system according to the fifth embodiment of the present invention; Figure 5B shows the spherical aberration, astigmatism, and optical distortion of the optical imaging system of the fifth embodiment of the present invention in order from left to right. Figure 5C shows the meridian of the optical imaging system of the fifth embodiment of the present invention. Surface light fan and sagittal light fan, the longest working wavelength and the shortest working wavelength are transverse aberration diagrams at the field of view of 0.7 through the edge of the aperture; Figure 5D shows the central field of view of the visible light spectrum of the fifth embodiment of the present invention, Defocus modulation conversion vs. transfer rate diagram for 0.3 field of view and 0.7 field of view; FIG. 5E is a diagram showing the central field of view, 0.3 field of view, and 0.7 field of view of the infrared light spectrum of the fifth embodiment of the present invention Contrast transfer rate chart; Figure 6A is a drawing Schematic diagram of the optical imaging system of the sixth embodiment of the invention; FIG. 6B shows the spherical aberration, astigmatism, and optical distortion of the optical imaging system of the sixth embodiment of the invention in order from left to right; A transverse aberration diagram of a meridional fan and a sagittal fan of a sixth embodiment of the optical imaging system of the present invention, with the longest working wavelength and the shortest working wavelength passing through the aperture edge at a field of view of 0.7; FIG. 6D is a drawing The sixth embodiment of the invention shows the central field of view of the visible light spectrum, 0.3 field of view, 0.7 field of view out of modulation modulation contrast transfer rate diagram; FIG. 6E is a diagram showing the central field of view of the infrared light spectrum of the sixth embodiment of the present invention , 0.3 field of view, Defocus modulation conversion vs. transfer rate plot for 0.7 field of view.

An optical imaging system group includes a first lens, a second lens, a third lens, and a fourth lens with refractive power in order from the object side to the image side. The optical imaging system may further include an image sensing element disposed on the imaging surface.

The optical imaging system can be designed using three working wavelengths, which are 486.1nm, 587.5nm, and 656.2nm, of which 587.5nm is the main reference wavelength and the reference wavelength for the main extraction technical features. The optical imaging system can also be designed using five working wavelengths, which are 470nm, 510nm, 555nm, 610nm, and 650nm, of which 555nm is the main reference wavelength and the reference wavelength for the main extraction technical features.

The ratio of the focal length f of the optical imaging system to the focal length fp of each lens with positive refractive power PPR, the ratio of the focal length f of the optical imaging system to the focal length fn of each lens with negative refractive power NPR, all lenses with positive refractive power The sum of PPR is ΣPPR, and the sum of NPR of all lenses with negative refractive power is ΣNPR. It helps to control the total refractive power and total length of the optical imaging system when the following conditions are met: 0.5 ≦ ΣPPR / ｜ ΣNPR ｜ ≦ 4.5, preferably The following conditions can be satisfied: 0.9 ≦ ΣPPR / | ΣNPR | ≦ 3.5.

The system height of the optical imaging system is HOS. When the HOS / f ratio approaches 1, it will be beneficial to make optical imaging systems that are miniaturized and capable of imaging ultra-high pixels.

The sum of the focal length fp of each lens with a positive refractive power is ΣPP, and the sum of the focal lengths of each lens with a negative refractive power is ΣNP. An embodiment of the optical imaging system of the present invention satisfies the following conditions: 0 <ΣPP ≦ 200; and f4 / ΣPP ≦ 0.85. Preferably, the following conditions can be satisfied: 0 <ΣPP ≦ 150; and 0.01 ≦ f4 / ΣPP ≦ 0.7. This helps to control the focusing ability of the optical imaging system, and appropriately distributes the positive refractive power of the system to prevent significant aberrations from occurring prematurely.

The optical imaging system may further include an image sensing element disposed on the imaging surface. The half of the diagonal length of the effective sensing area of the image sensing element (that is, the imaging height or maximum image height of the optical imaging system) is HOI. The distance from the side of the first lens object to the imaging surface on the optical axis is HOS. The following conditions are satisfied: HOS / HOI ≦ 15; and 0.5 ≦ HOS / f ≦ 20.0. Preferably, the following conditions can be satisfied: 1 ≦ HOS / HOI ≦ 10; and 1 ≦ HOS / f ≦ 15. By this, the optical can be maintained The miniaturization of the imaging system to be mounted on thin and light portable electronic products.

In addition, in the optical imaging system of the present invention, at least one aperture can be set as required to reduce stray light and help improve image quality.

In the optical imaging system of the present invention, the aperture configuration may be a front aperture or a middle aperture, wherein the front aperture means that the aperture is set between the subject and the first lens, and the middle aperture means that the aperture is set between the first lens and the first lens. Between imaging surfaces. If the aperture is a front aperture, it can make the exit pupil of the optical imaging system and the imaging surface have a longer distance to accommodate more optical elements, and increase the efficiency of the image sensing element to receive images; if it is a middle aperture, the system It helps to expand the field of view of the system, so that the optical imaging system has the advantages of a wide-angle lens. The distance from the aforementioned aperture to the imaging surface is InS, which satisfies the following conditions: 0.2 ≦ InS / HOS ≦ 1.1. Preferably, the following conditions can be satisfied: 0.4 ≦ InS / HOS ≦ 1, thereby maintaining both the miniaturization of the optical imaging system and the characteristics of having a wide angle.

In the optical imaging system of the present invention, the distance between the object side of the first lens and the image side of the fourth lens is InTL, and the sum of the thicknesses of all lenses with refractive power on the optical axis ΣTP, which satisfies the following conditions: 0.2 ≦ ΣTP / InTL ≦ 0.95. Preferably, the following conditions can be satisfied: 0.2 ≦ ΣTP / InTL ≦ 0.9. Thereby, the contrast of the system imaging and the yield of lens manufacturing can be taken into account at the same time, and an appropriate back focus can be provided to accommodate other components.

The curvature radius of the object side of the first lens is R1, and the curvature radius of the image side of the first lens is R2, which satisfies the following conditions: 0.01 ≦ | R1 / R2 | ≦ 100. Preferably, the following conditions can be satisfied: 0.01 ≦ | R1 / R2 | ≦ 60.

The curvature radius of the object side of the fourth lens is R9, and the curvature radius of the image side of the fourth lens is R10, which satisfies the following conditions: -200 <(R7-R8) / (R7 + R8) <30. This is beneficial to correct the astigmatism generated by the optical imaging system.

The distance between the first lens and the second lens on the optical axis is IN12, which satisfies the following conditions: 0 <IN12 / f ≦ 5.0. Preferably, the following conditions can be satisfied: 0.01 ≦ IN12 / f ≦ 4.0. This helps to improve the chromatic aberration of the lens to improve its performance.

The distance between the second lens and the third lens on the optical axis is IN23, which satisfies the following conditions: 0 <IN23 / f ≦ 5.0. Preferably, the following conditions can be satisfied: 0.01 ≦ IN23 / f ≦ 3.0. This helps to improve the performance of the lens.

The distance between the third lens and the fourth lens on the optical axis is IN34, which satisfies the following conditions: 0 <IN34 / f ≦ 5.0. Preferably, the following conditions can be satisfied: 0.001 ≦ IN34 / f ≦ 3.0. This helps to improve the performance of the lens.

The thicknesses of the first lens and the second lens on the optical axis are respectively TP1 and TP2, which satisfy the following conditions: 1 ≦ (TP1 + IN12) / TP2 ≦ 20. This helps to control the sensitivity of the optical imaging system manufacturing and improve its performance.

The thicknesses of the third lens and the fourth lens on the optical axis are TP3 and TP4, respectively. The distance between the two lenses on the optical axis is IN34, which satisfies the following conditions: 0.2 ≦ (TP4 + IN34) / TP4 ≦ 20. This helps to control the sensitivity of the optical imaging system manufacturing and reduce the overall system height.

The distance between the second lens and the third lens on the optical axis is IN23, and the total distance between the first lens and the fourth lens on the optical axis is ΣTP, which satisfies the following conditions: 0.01 ≦ IN23 / (TP2 + IN23 + TP3) ≦ 0.9. Preferably, the following conditions can be satisfied: 0.05 ≦ IN23 / (TP2 + IN23 + TP3) ≦ 0.7. This helps the layers to slightly correct the aberrations generated by the incident light traveling and reduce the overall system height.

In the optical imaging system of the present invention, the horizontal displacement distance of the fourth lens objective side surface 142 on the optical axis to the maximum effective radius position of the fourth lens objective side surface 142 on the optical axis is InRS41 (if the horizontal displacement is toward the image side, InRS41 Is a positive value; if the horizontal displacement is toward the object side, InRS41 is a negative value), the horizontal lens displacement distance of the fourth lens image side 144 on the optical axis to the maximum effective radius position of the fourth lens image side 144 on the optical axis is InRS42 The thickness of the fourth lens 140 on the optical axis is TP4, which meets the following conditions: -1mm ≦ InRS41 ≦ 1mm; -1mm ≦ InRS42 ≦ 1mm; 1mm ≦ | InRS41 | + | InRS42 | ≦ 2mm; 0.01 ≦ | InRS41 | / TP4 ≦ 10; 0.01 ≦ | InRS42 | / TP4 ≦ 10. Thereby, the position of the maximum effective radius between the two surfaces of the fourth lens can be controlled, which contributes to aberration correction of the peripheral field of view of the optical imaging system and effectively maintains its miniaturization.

In the optical imaging system of the present invention, the horizontal displacement distance parallel to the optical axis between the intersection point of the fourth lens object side on the optical axis and the closest optical axis inflection point of the fourth lens object side is represented by SGI411. The fourth lens image The horizontal displacement distance parallel to the optical axis from the intersection of the side on the optical axis to the closest optical axis of the fourth lens image side is represented by SGI421, which satisfies the following conditions: 0 <SGI411 / (SGI411 + TP4) ≦ 0.9 ; 0 <SGI421 / (SGI421 + TP4) ≦ 0.9. Preferably, the following conditions can be satisfied: 0.01 <SGI411 / (SGI411 + TP4) ≦ 0.7; 0.01 <SGI421 / (SGI421 + TP4) ≦ 0.7.

The horizontal displacement distance parallel to the optical axis between the intersection of the object side of the fourth lens on the optical axis and the second inflection point of the object side of the fourth lens close to the optical axis is represented by SGI412. The image side of the fourth lens on the optical axis The horizontal displacement distance parallel to the optical axis between the intersection point and the inflection point of the fourth lens image side close to the optical axis is represented by SGI422, which satisfies the following conditions: 0 <SGI412 / (SGI412 + TP4) ≦ 0.9; 0 <SGI422 /(SGI422+TP4)≦0.9. Preferably, the following conditions can be satisfied: 0.1 ≦ SGI412 / (SGI412 + TP4) ≦ 0.8; 0.1 ≦ SGI422 / (SGI422 + TP4) ≦ 0.8.

The vertical distance between the inflection point of the closest optical axis of the fourth lens object side and the optical axis is represented by HIF411. The intersection point of the fourth lens image side on the optical axis to the closest optical axis of the fourth lens image side and the inflection point of the optical axis The vertical distance between them is represented by HIF421, which satisfies the following conditions: 0.01 ≦ HIF411 / HOI ≦ 0.9; 0.01 ≦ HIF421 / HOI ≦ 0.9. Preferably, the following conditions can be satisfied: 0.09 ≦ HIF411 / HOI ≦ 0.5; 0.09 ≦ HIF421 / HOI ≦ 0.5.

The vertical distance between the second inflection point of the fourth lens object side close to the optical axis and the optical axis is represented by HIF412. The intersection of the fourth lens image side on the optical axis to the second lens image side second inflection near the optical axis The vertical distance between the point and the optical axis is represented by HIF422, which satisfies the following conditions: 0.01 ≦ HIF412 / HOI ≦ 0.9; 0.01 ≦ HIF422 / HOI ≦ 0.9. Preferably, the following conditions can be satisfied: 0.09 ≦ HIF412 / HOI ≦ 0.8; 0.09 ≦ HIF422 / HOI ≦ 0.8.

The vertical distance between the inflection point of the fourth lens object side close to the optical axis and the optical axis is represented by HIF413, and the intersection of the fourth lens image side on the optical axis to the third lens image side of the third lens close to the optical axis. The vertical distance between the point and the optical axis is represented by HIF423, which satisfies the following conditions: 0.001mm ≦ | HIF413 | ≦ 5mm; 0.001mm ≦ | HIF423 | ≦ 5mm. Preferably, the following conditions can be satisfied: 0.1mm ≦ | HIF423 | ≦ 3.5mm; 0.1mm ≦ | HIF413 | ≦ 3.5mm.

The vertical distance between the inflection point of the fourth lens object side close to the optical axis and the optical axis is represented by HIF414. The intersection of the fourth lens image side on the optical axis to the fourth lens image side is the fourth curve close to the optical axis. The vertical distance between the point and the optical axis is represented by HIF424, which satisfies the following conditions: 0.001mm ≦ | HIF414 | ≦ 5mm; 0.001mm ≦ | HIF424 | ≦ 5mm. Preferably, the following conditions can be satisfied: 0.1mm ≦ | HIF424 | ≦ 3.5mm; 0.1mm ≦ | HIF414 | ≦ 3.5mm.

According to an embodiment of the optical imaging system of the present invention, a high color The staggered and low-dispersion lenses are staggered to help correct the chromatic aberration of the optical imaging system.

The equation of the above aspheric surface is: z = ch ² / [1+ [1 (k + 1) c ² h ² ] ^0.5 ] + A4h ⁴ + A6h ⁶ + A8h ⁸ + A10h ¹⁰ + A12h ¹² + A14h ¹⁴ + A16h ¹⁶ + A18h ¹⁸ + A20h ²⁰ + ... (1) where z is the position value with the surface vertex as the reference at the position of height h along the optical axis direction, k is the cone surface coefficient, and c is the inverse of the radius of curvature, And A4, A6, A8, A10, A12, A14, A16, A18, and A20 are high-order aspheric coefficients.

In the optical imaging system provided by the present invention, the material of the lens may be plastic or glass. When the lens is made of plastic, it can effectively reduce production costs and weight. In addition, when the material of the lens is glass, the thermal effect can be controlled and the design space of the refractive power configuration of the optical imaging system can be increased. In addition, the object side and the image side of the first lens to the fourth lens in the optical imaging system can be aspheric, which can obtain more control variables. In addition to reducing aberrations, compared with the use of traditional glass lenses, The number of lenses used can be reduced, so the overall height of the optical imaging system of the present invention can be effectively reduced.

Furthermore, in the optical imaging system provided by the present invention, if the lens surface is convex, it means that the lens surface is convex at the near optical axis; if the lens surface is concave, it means that the lens surface is concave at the low optical axis.

In addition, in the optical imaging system of the present invention, at least one light bar may be provided according to requirements to reduce stray light and help improve image quality.

The optical imaging system of the present invention can be applied to an optical system for mobile focusing as required, and has both the characteristics of excellent aberration correction and good imaging quality, thereby expanding the application level.

The optical imaging system of the present invention may further include a driving module as required. The driving module may be coupled to the lenses and cause the lenses to be displaced. The aforementioned driving module may be a voice coil motor (VCM) for driving the lens to focus, or an optical anti-shake element (OIS) for reducing the frequency of out-of-focus caused by lens vibration during shooting.

According to the optical imaging system of the present invention, at least one of the first lens, the second lens, the third lens, and the fourth lens may be a light filtering element with a wavelength less than 500 nm according to the requirements. At least one surface of the lens is coated or the lens itself is made of a material capable of filtering out short wavelengths.

According to the above embodiments, specific examples are provided below and given in conjunction with the drawings. Detailed description.

First embodiment

Please refer to FIG. 1A and FIG. 1B, wherein FIG. 1A shows a schematic diagram of an optical imaging system according to the first embodiment of the present invention, and FIG. 1B shows the optical imaging system of the first embodiment in order from left to right. Spherical aberration, astigmatism and optical distortion curves. FIG. 1C is a transverse aberration diagram of the meridional fan and the sagittal fan of the optical imaging system of the first embodiment at the longest working wavelength and the shortest working wavelength through the aperture edge at a field of view of 0.7. FIG. 1D is a diagram showing the center-of-view, 0.3-field, and 0.7-field defocus modulation conversion contrast transfer rate diagrams of the visible light spectrum according to the embodiment of the present invention; FIG. 1E is a first focus of the present invention. Defocus modulation conversion vs. transfer rate diagram for the central field of view, 0.3 field of view, and 0.7 field of view of the infrared light spectrum of the embodiment. As can be seen from FIG. 1A, the optical imaging system includes a first lens 110, a second lens 120, an aperture 100, a third lens 130, a fourth lens 140, an infrared filter 170, and an imaging surface 180 in this order from the object side to the image side. And image sensing element 190.

The first lens 110 has a negative refractive power and is made of glass. The object side 112 is convex, the image side 114 is concave, and both are aspheric. The length of the contour curve of the maximum effective radius on the object side of the first lens is represented by ARS11, and the length of the contour curve of the maximum effective radius of the image side of the first lens is represented by ARS12. The length of the contour curve of the 1/2 incident pupil diameter (HEP) on the object side of the first lens is represented by ARE11, and the length of the contour curve of the 1/2 incidence pupil diameter (HEP) of the first lens image side is represented by ARE12. The thickness of the first lens on the optical axis is TP1.

The horizontal displacement distance parallel to the optical axis between the intersection of the object side of the first lens on the optical axis and the closest optical axis inflection point of the object side of the first lens is represented by SGI111. The intersection of the image side of the first lens on the optical axis to The horizontal displacement distance between the inflection points of the closest optical axis of the first lens image side parallel to the optical axis is represented by SGI121, which satisfies the following conditions: SGI111 = 0mm; SGI121 = 0mm; | SGI111 ｜ / (｜ SGI111 ｜ + TP1) = 0; | SGI121 | / (｜ SGI121 | + TP1) = 0.

The vertical distance between the intersection of the object lens's side surface on the optical axis and the closest optical axis's inflection point on the object side of the first lens and the optical axis is represented by HIF111. The intersection of the image side of the first lens on the optical axis to the first lens The vertical distance between the inflection point of the closest optical axis on the side of the mirror and the optical axis is represented by HIF121, which meets the following conditions: HIF111 = 0mm; HIF121 = 0mm; HIF111 / HOI = 0; HIF121 / HOI = 0.

The second lens 120 has a positive refractive power and is made of plastic. The object side surface 122 is concave, the image side surface 124 is convex, and both are aspheric. The object side surface 122 has a inflection point. The length of the contour curve of the maximum effective radius on the object side of the second lens is represented by ARS21, and the length of the contour curve of the maximum effective radius of the image side of the second lens is represented by ARS22. The length of the profile curve of 1/2 incident pupil diameter (HEP) on the object side of the second lens is represented by ARE21, and the length of the profile curve of 1/2 incident pupil diameter (HEP) on the image side of the second lens is represented by ARE22. The thickness of the second lens on the optical axis is TP2.

The horizontal displacement distance parallel to the optical axis between the intersection point of the second lens object side on the optical axis and the closest optical axis inflection point of the second lens object side is represented by SGI211. The intersection point of the second lens image side on the optical axis is The horizontal displacement distance between the inflection points of the closest optical axis of the second lens image side parallel to the optical axis is represented by SGI221, which satisfies the following conditions: SGI211 = -0.13283mm; ｜ SGI211 ｜ / (｜ SGI211 ｜ + TP2) = 0.05045 .

The vertical distance between the intersection of the second lens object side on the optical axis and the closest optical axis of the second lens object side to the inflection point and the optical axis is represented by HIF211. The intersection of the second lens image side on the optical axis to the second lens The vertical distance between the inflection point of the closest optical axis on the side of the mirror and the optical axis is represented by HIF221, which meets the following conditions: HIF211 = 2.10379mm; HIF211 / HOI = 0.69478.

The third lens 130 has a negative refractive power and is made of plastic. Its object side surface 132 is concave, its image side 134 is concave, and both are aspheric. The image side 134 has a point of inflection. The length of the contour curve of the maximum effective radius on the object side of the third lens is represented by ARS31, and the length of the contour curve of the maximum effective radius of the image side of the third lens is represented by ARS32. The length of the contour curve of 1/2 incident pupil diameter (HEP) on the object side of the third lens is represented by ARE31, and the length of the contour curve of 1/2 incident pupil diameter (HEP) on the image side of the third lens is represented by ARE32. The thickness of the third lens on the optical axis is TP3.

The horizontal displacement distance parallel to the optical axis between the intersection point of the third lens object side on the optical axis and the closest optical axis inflection point of the third lens object side is represented by SGI311. The intersection point of the third lens image side on the optical axis is The horizontal displacement distance between the inflection points of the closest optical axis of the third lens image side parallel to the optical axis is represented by SGI321, which satisfies the following conditions: SGI321 = 0.01218mm; | SGI321 | / (｜ SGI321 | + TP3) = 0.03902.

The vertical distance between the inflection point of the closest optical axis of the third lens object side and the optical axis is represented by HIF311. The intersection of the third lens image side on the optical axis to the closest optical axis of the third lens image side The vertical distance between the inflection point and the optical axis is represented by HIF321, which meets the following conditions: HIF321 = 0.84373mm; HIF321 / HOI = 0.27864.

The fourth lens 140 has a positive refractive power and is made of plastic. Its object side surface 142 is convex, its image side 144 is convex, and both are aspheric. The image side 144 has a point of inflection. The length of the contour curve of the maximum effective radius on the object side of the fourth lens is represented by ARS41, and the length of the contour curve of the maximum effective radius of the image side of the fourth lens is represented by ARS42. The length of the contour curve of the 1/2 incident pupil diameter (HEP) on the object side of the fourth lens is represented by ARE41, and the length of the contour curve of the 1/2 incidence pupil diameter (HEP) of the fourth lens image side is represented by ARE42. The thickness of the fourth lens on the optical axis is TP4.

The horizontal displacement distance parallel to the optical axis between the intersection point of the fourth lens object side on the optical axis and the closest optical axis inflection point of the fourth lens object side is represented by SGI411. The intersection point of the fourth lens image side on the optical axis is The horizontal displacement distance between the inflection points of the closest optical axis of the fourth lens image side parallel to the optical axis is represented by SGI421, which satisfies the following conditions: SGI411 = 0mm; SGI421 = -0.41627mm; | SGI411 ｜ / (｜ SGI411 ｜ + TP4) = 0; | SGI421 | / (| SGI421 | + TP4) = 0.25015.

The horizontal displacement distance parallel to the optical axis between the intersection point of the fourth lens object side on the optical axis and the second curved point near the optical axis of the fourth lens object side is represented by SGI412, which satisfies the following conditions: SGI412 = 0mm; SGI412 ｜ / (｜ SGI412 ｜ + TP4) = 0.

The vertical distance between the inflection point of the closest optical axis on the object side of the fourth lens and the optical axis is represented by HIF411, and the vertical distance between the inflection point of the closest optical axis on the side of the fourth lens image and the optical axis is HIF411, which satisfies the following conditions : HIF411 = 0mm; HIF421 = 1.55079mm; HIF411 / HOI = 0; HIF421 / HOI = 0.51215.

The vertical distance between the inflection point of the second near-beam axis on the object side of the fourth lens and the optical axis is represented by HIF412, which satisfies the following conditions: HIF412 = 0mm; HIF412 / HOI = 0.

The infrared filter 170 is made of glass and is disposed between the fourth lens 140 and the imaging surface 180 without affecting the focal length of the optical imaging system.

In the optical imaging system of the first embodiment, the focal length of the optical imaging system is f, the entrance pupil diameter of the optical imaging system is HEP, and the half of the maximum viewing angle in the optical imaging system is HAF, and the value is as follows: f = 2.6841mm; f / HEP = 2.7959; and HAF = 70 degrees and tan (HAF) = 2.7475.

In the optical imaging system of the first embodiment, the focal length of the first lens 110 is f1 and the focal length of the fourth lens 140 is f4, which satisfies the following conditions: f1 = -5.4534mm; | f / f1 | = 0.4922; f4 = 2.7595 mm; and | f1 / f4 | = 1.9762.

In the optical imaging system of the first embodiment, the focal lengths of the second lens 120 to the third lens 130 are f2 and f3, which satisfy the following conditions: | f2 | + | f3 | = 13.62561mm; | f1 | + | f4 | = 8.2129mm and | f2 | + | f3 |> | f1 | + | f4 |.

The ratio of the focal length f of the optical imaging system to the focal length fp of each lens with a positive refractive power, PPR, and the ratio of the focal length f of the optical imaging system to the focal length fn of each lens with a negative refractive power, NPR. In the imaging system, the sum of PPR of all lenses with positive refractive power is ΣPPR = | f / f2 | + | f / f4 | = 1.25394, and the sum of NPR of all lenses with negative refractive power is ΣNPR = | f / f1 | + | f /f2｜=1.21490, ΣPPR / ｜ ΣNPR ｜ = 1.03213. The following conditions are also met: | f / f1 | = 0.49218; | f / f2 | = 0.28128; | f / f3 | = 0.72273; | f / f4 | = 0.97267.

In the optical imaging system of the first embodiment, the distance between the first lens object side 112 to the fourth lens image side 144 is InTL, the distance between the first lens object side 112 to the imaging surface 180 is HOS, and the aperture 100 to the imaging surface The distance between 180 is InS, half of the diagonal length of the effective sensing area of the image sensing element 190 is HOI, and the distance between the image side 144 of the fourth lens and the imaging surface 180 is InB, which meets the following conditions: InTL + InB = HOS; HOS = 18.74760mm; HOI = 3.088mm; HOS / HOI = 6.19141; HOS / f = 6.9848; InTL / HOS = 0.6605; InS = 8.2310mm; and InS / HOS = 0.4390.

In the optical imaging system of the first embodiment, the total thickness of all the lenses with refractive power on the optical axis is ΣTP, which satisfies the following conditions: ΣTP = 4.9656mm; and ΣTP / InTL = 0.4010. Thereby, the contrast of the system imaging and the yield of lens manufacturing can be taken into account at the same time, and an appropriate back focus can be provided to accommodate other components.

In the optical imaging system of the first embodiment, the curvature radius of the object side surface 112 of the first lens is R1, and the curvature radius of the image side 114 of the first lens is R2, which satisfies the following conditions: | R1 / R2 | = 9.6100. Thereby, the first lens has an appropriate positive refractive power strength, and avoids an increase in spherical aberration from overspeed.

In the optical imaging system of the first embodiment, the curvature radius of the object side surface 142 of the fourth lens is R7, and the curvature radius of the image side surface 144 of the fourth lens is R8, which satisfies the following conditions: (R7-R8) / (R7 + R8) =-35.5932. This is beneficial to correct the astigmatism generated by the optical imaging system.

In the optical imaging system of the first embodiment, the sum of the focal lengths of all the lenses with positive refractive power is ΣPP, which satisfies the following conditions: ΣPP = 12.30183mm; and f4 / ΣPP = 0.22432. Therefore, it is helpful to appropriately allocate the positive refractive power of the fourth lens 140 to other positive lenses, so as to suppress the occurrence of significant aberrations during the traveling process of incident light.

In the optical imaging system of the first embodiment, the sum of the focal lengths of all the lenses with negative refractive power is ΣNP, which satisfies the following conditions: ΣNP = -14.6405mm; and f1 / ΣNP = 0.59488. This helps to appropriately distribute the negative refractive power of the fourth lens to other negative lenses, so as to suppress the occurrence of significant aberrations during the traveling process of incident light.

In the optical imaging system of the first embodiment, the distance between the first lens 110 and the second lens 120 on the optical axis is IN12, which satisfies the following conditions: IN12 = 4.5709mm; IN12 / f = 1.70299. This helps to improve the chromatic aberration of the lens to improve its performance.

In the optical imaging system of the first embodiment, the distance between the second lens 120 and the third lens 130 on the optical axis is IN23, which satisfies the following conditions: IN23 = 2.7524mm; IN23 / f = 1.02548. This helps to improve the chromatic aberration of the lens to improve its performance.

In the optical imaging system of the first embodiment, the distance between the third lens 130 and the fourth lens 140 on the optical axis is IN34, which satisfies the following conditions: IN34 = 0.0944mm; IN34 / f = 0.03517. This helps to improve the chromatic aberration of the lens to improve its performance.

In the optical imaging system of the first embodiment, the thicknesses of the first lens 110 and the second lens 120 on the optical axis are TP1 and TP2, respectively, which satisfy the following conditions: TP1 = 0.9179mm; TP2 = 2.5000mm; TP1 / TP2 = 0.36715 and (TP1 + IN12) /TP2=2.19552. This helps to control the sensitivity of the optical imaging system manufacturing and improve its performance.

In the optical imaging system of the first embodiment, the thicknesses of the third lens 130 and the fourth lens 140 on the optical axis are TP3 and TP4, and the distance between the two lenses on the optical axis is IN34, which meets the following conditions: TP3 = 0.3mm; TP4 = 1.2478mm; TP3 / TP4 = 0.24043 and (TP4 + IN34) /TP3=4.47393. This helps to control the sensitivity of the optical imaging system manufacturing and reduce the overall system height.

In the optical imaging system of the first embodiment, it satisfies the following conditions: IN23 / (TP2 + IN23 + TP3) = 0.49572. This helps to slightly modify the travel process of incident light. The resulting aberrations and reduce the overall height of the system.

In the optical imaging system of the first embodiment, the horizontal displacement distance from the intersection of the fourth lens object side surface 142 on the optical axis to the maximum effective radius position of the fourth lens object side surface 142 on the optical axis is InRS41, and the fourth lens image side 144 The horizontal displacement distance from the intersection point on the optical axis to the maximum effective radius position of the fourth lens image side 144 on the optical axis is InRS42. The thickness of the fourth lens 140 on the optical axis is TP4, which meets the following conditions: InRS41 = 0.2955mm ; InRS42 = -0.4940mm; | InRS41 | + | InRS42 | = 0.7894mm; | InRS41 | /TP4=0.23679; and | InRS42 | /TP4=0.39590. This facilitates lens manufacturing and molding, and effectively maintains its miniaturization.

In the optical imaging system of this embodiment, the vertical distance between the critical point C41 of the fourth lens object side 142 and the optical axis is HVT41, and the vertical distance between the critical point C42 of the fourth lens image side 144 and the optical axis is HVT42, which satisfies the following Conditions: HVT41 = 0mm; HVT42 = 0mm.

The optical imaging system of this embodiment satisfies the following conditions: HVT42 / HOI = 0.

The optical imaging system of this embodiment satisfies the following conditions: HVT42 / HOS = 0.

In the optical imaging system of the first embodiment, the dispersion coefficient of the first lens is NA1, the dispersion coefficient of the second lens is NA2, the dispersion coefficient of the third lens is NA3, and the dispersion coefficient of the fourth lens is NA4, which satisfies the following conditions : | NA1-NA2 | = 0.0351. This helps to correct the chromatic aberration of the optical imaging system.

In the optical imaging system of the first embodiment, the TV distortion of the optical imaging system during the image formation is TDT and the optical distortion during the image formation is ODT, which satisfies the following conditions: TDT = 37.4846%; ODT = -55.3331%.

The light in any field of view of the embodiment of the present invention can be further divided into sagittal ray and tangential ray, and the evaluation basis of the focus offset and MTF value is a spatial frequency of 220 cycles / mm. The focus offsets of the maximum defocus MTF of the sagittal rays of the visible central field of view, 0.3 fields of view, and 0.7 fields of view are represented by VSFS0, VSFS3, and VSFS7 (measurement units: mm), and the values are 0.00000mm and 0.0000, respectively. mm, 0.00000mm; the maximum value of the defocus MTF of the sagittal rays of the central field of view, 0.3 field of view, and 0.7 field of view is represented by VSMTF0, VSMTF3, and VSMTF7, and the values are 0.416, 0.397, and 0.342; the central field of view of visible light Defocus of the meridional light of 0.3, 0.7 and 0.7 fields of view The focus offset of the maximum MTF is represented by VTFS0, VTFS3, and VTFS7 (unit of measurement: mm), and the values are 0.00000mm, 0.00000mm, and -0.01000mm, respectively; the center of view of the visible light, 0.3 and 0.7 The maximum out-of-focus MTF of the meridian rays is represented by VTMTF0, VTMTF3, and VTMTF7, and the values are 0.416, 0.34, and 0.139, respectively. The average focus shift amount (position) of the focus shift amounts of the aforementioned sagittal three-view field of the visible arc and the meridional three-view field of visible light is represented by AVFS (measurement unit: mm), which satisfies the absolute value | VTFS0 + VTFS3 + VTFS7) / 6 ｜ = ｜ -0.00200mm ｜.

In this embodiment, the focus offsets of the maximum defocus MTF of the sagittal rays of the central field of view, the field of view of 0.3, and the field of view of 0.7 are represented by ISFS0, ISFS3, and ISFS7 (unit of measurement: mm), and the values are respectively It is 0.03000mm, 0.03300mm, 0.03300mm. The average focus offset (position) of the aforementioned three focus fields of sagittal plane is represented by AISFS; the center of the infrared light field, 0.3 field of view, 0.7 field of sagittal plane The maximum defocus MTF of the light is represented by ISMTF0, ISMTF3, and ISMTF7, and the values are 0.169, 0.148, and 0.089 respectively; the maximum defocus MTF of the meridional rays of the central light field, 0.3 field of view, and 0.7 field of infrared light The focus offsets are respectively represented by ITFS0, ITFS3, and ITFS7 (units of measurement: mm), and their values are 0.03, 0.028, and 0.005, respectively. The average focus offset (position) of the aforementioned three-field meridional focus offsets is AITFS (measurement unit: mm); the maximum defocus MTF of the meridional rays of the central field, 0.3 field of view, and 0.7 field of view of the infrared light is represented by IMTTF0, IMTTF3, and IMTTF7, and the values are 0.169, 0.093, and 0.0000, respectively. . The average focus offset (position) of the aforementioned infrared light sagittal three-field and infrared light meridional three-field is represented by AIFS (unit of measurement: mm), which satisfies the absolute value | (ISFS0 + ISFS3 + ISFS7 + ITFS0 + ITFS3 + ITFS7) / 6 ｜ = ｜ 0.02600mm ｜.

The focus offset between the visible light center field focus point and the infrared light center field focus point (RGB / IR) of the entire optical imaging system in this embodiment is represented by FS (that is, a wavelength of 850 nm to a wavelength of 555 nm, a unit of measurement: mm) , Which satisfies the absolute value ｜ (VSFS0 + VTFS0) / 2- (ISFS0 + ITFS0) / 2 ｜ = ｜ 0.03000mm ｜; the visible focus three-field average focus offset and infrared light three-field average focus of the entire optical imaging system The difference between the offsets (RGB / IR) (focus offset) is expressed in AFS (ie, wavelength 850nm vs. wavelength 555nm, unit of measurement: mm), which satisfies the absolute value | AIFS-AVFS | = | 0.02800mm | .

In the optical imaging system of this embodiment, the longest time The transverse aberration of 0.7 field of view incident on the imaging surface through the edge of the aperture is expressed in PLTA, which is -0.018mm. The shortest working wavelength of the positive meridional fan diagram is incident on the imaging plane through the edge of the aperture. The lateral aberration is represented by PSTA, which is 0.010mm. The longest working wavelength of the negative meridional fan diagram is incident on the imaging surface through the aperture edge. The lateral aberration of 0.7 field of view is represented by NLTA, which is 0.003mm, negative meridian. The shortest working wavelength of the surface light fan diagram is 0.7 mm. The lateral aberration of the 0.7 field of view incident on the imaging surface through the edge of the aperture is -0.003mm. The longest working wavelength of the sagittal plane fan chart is incident on the imaging plane through the aperture edge. The transverse aberration of 0.7 field of view is expressed by SLTA, which is -0.010mm. The shortest working wavelength of the sagittal plane fan chart is incident on the imaging plane through the diaphragm edge. The lateral aberration of the upper 0.7 field of view is represented by SSTA, which is 0.003 mm.

Refer to Tables 1 and 2 below for further cooperation.

According to Table 1 and Table 2, the relevant values of the contour curve length can be obtained:

Table 1 shows the detailed structural data of the first embodiment in FIG. 1, where the units of the radius of curvature, thickness, distance, and focal length are mm, and the surface 0-14 sequentially represents the surface from the object side to the image side. Table 2 shows the aspheric data in the first embodiment, where k represents the cone coefficient in the aspheric curve equation, and A1-A20 represents the aspherical coefficients of order 1-20 on each surface. In addition, the tables of the following embodiments are schematic diagrams and aberration curves corresponding to the embodiments. The definitions of the data in the tables are the same as the definitions of Tables 1 and 2 of the first embodiment, and will not be repeated here.

Second embodiment

Please refer to FIG. 2A and FIG. 2B, wherein FIG. 2A shows a schematic diagram of an optical imaging system according to a second embodiment of the present invention, and FIG. 2B shows the optical imaging system of the second embodiment in order from left to right. Spherical aberration, astigmatism and optical distortion curves. Figure 2C is an optical imaging system of the second embodiment The horizontal aberration diagram of the traditional meridional fan and sagittal fan, the longest working wavelength and the shortest working wavelength pass through the edge of the aperture at a field of view of 0.7. FIG. 2D is a diagram showing the defocus modulation conversion contrast transfer rate of the central field of view, 0.3 field of view, and 0.7 field of view of the visible light spectrum of the second embodiment of the present invention; FIG. 2E is a view of the second embodiment of the present invention. Defocus modulation conversion vs. transfer rate diagram for the central field of view, 0.3 field of view, and 0.7 field of view of the infrared light spectrum. It can be seen from FIG. 2A that the optical imaging system includes a first lens 210, an aperture 200, a second lens 220, a third lens 230, a fourth lens 240, an infrared filter 270, and an imaging surface 280 in order from the object side to the image side. And an image sensing element 290.

The first lens 210 has a negative refractive power and is made of plastic. The object side surface 212 is convex, the image side 214 is concave, and both are aspheric. The object side 212 and the image side 214 each have an inflection point.

The second lens 220 has a positive refractive power and is made of plastic material. Its object side surface 222 is convex, its image side surface 224 is convex, and both are aspheric, and its object side surface 222 has an inflection point.

The third lens 230 has a positive refractive power and is made of plastic. Its object side surface 232 is concave, its image side 234 is convex, and both are aspheric. Both its object side 232 and image side 234 have an inflection point.

The fourth lens 240 has a negative refractive power and is made of plastic. Its object-side surface 242 is convex, its image-side 244 is concave, and both are aspheric, and its object-side 242 and image-side 244 both have an inflection point.

The infrared filter 270 is made of glass and is disposed between the fourth lens 240 and the imaging surface 280 without affecting the focal length of the optical imaging system.

In the optical imaging system of the second embodiment, the second lens and the third lens are positive lenses, and their individual focal lengths are f2 and f3 respectively. The sum of the focal lengths of all lenses with positive refractive power is ΣPP, which meets the following conditions: ΣPP = f2 + f3. This helps to properly distribute the positive refractive power of a single lens to other positive lenses, so as to suppress the occurrence of significant aberrations during the traveling of incident light.

In the optical imaging system of the second embodiment, the sum of the focal lengths of all the lenses with negative refractive power is ΣNP, which satisfies the following conditions: ΣNP = f1 + f3.

Please refer to Tables 3 and 4 below.

In the second embodiment, the aspherical curve equation is expressed as the first embodiment. In addition, the definitions of the parameters in the following table are the same as those in the first embodiment, and will not be repeated here.

According to Table 3 and Table 4, the following conditional formula values can be obtained:

According to Table 3 and Table 4, the following conditional formula values can be obtained:

The values related to the length of the contour curve can be obtained according to Tables 3 and 4.

Third embodiment

Please refer to FIG. 3A and FIG. 3B, wherein FIG. 3A shows a schematic diagram of an optical imaging system according to a third embodiment of the present invention, and FIG. 3B shows the optical imaging system of the third embodiment in order from left to right. Spherical aberration, astigmatism and optical distortion curves. FIG. 3C is a transverse aberration diagram of the meridional fan and the sagittal fan of the optical imaging system according to the third embodiment, with the longest working wavelength and the shortest working wavelength passing through the aperture edge at a field of view of 0.7. Fig. 3D is a diagram showing the defocus modulation conversion contrast transfer rate of the central field of view, 0.3 field of view, and 0.7 field of view of the visible light spectrum of the third embodiment of the present invention; and Fig. 3E is a view of the third embodiment of the present invention. Defocus modulation conversion vs. transfer rate diagram for the central field of view, 0.3 field of view, and 0.7 field of view of the infrared light spectrum. As can be seen from FIG. 3A, the optical imaging system includes a first lens 310, an aperture 300, a second lens 320, a third lens 330, a fourth lens 340, an infrared filter 370, and an imaging surface 380 in order from the object side to the image side. And image sensing element 390.

The first lens 310 has a positive refractive power and is made of plastic. The object side 312 is convex, the image side 314 is concave, and both are aspheric. The object side 312 and the image side 314 each have a point of inflection.

The second lens 320 has a positive refractive power and is made of plastic. The object side surface 322 is convex, the image side 324 is convex, and both are aspheric. The object side 322 and the image side 324 each have an inflection point.

The third lens 330 has a positive refractive power and is made of plastic. The object side surface 332 is concave, the image side surface 334 is convex, and both are aspheric. The object side surface 332 and the image side 334 each have a point of inflection.

The fourth lens 340 has a negative refractive power and is made of plastic. The object side surface 342 is convex, the image side 344 is concave, and both are aspheric. The object side 342 and the image side 344 both have an inflection point.

The infrared filter 370 is made of glass and is disposed between the fourth lens 340 and the imaging surface 380 without affecting the focal length of the optical imaging system.

In the optical imaging system of the third embodiment, the first lens, the second lens, and the third lens are all positive lenses, and their individual focal lengths are f1, f2, and f3, and the sum of the focal lengths of all lenses with positive refractive power is ΣPP, It satisfies the following conditions: ΣPP = f1 + f2 + f3. This helps to properly distribute the positive refractive power of a single lens to other positive lenses, so as to suppress the occurrence of significant aberrations during the traveling of incident light.

In the optical imaging system of the third embodiment, the sum of the focal lengths of all the lenses with negative refractive power is ΣNP, which satisfies the following conditions: ΣNP = f4.

Please refer to Table 5 and Table 6 below.

In the third embodiment, the aspherical curve equation is expressed as the first embodiment. In addition, the definitions of the parameters in the following table are the same as those in the first embodiment, and will not be repeated here.

According to Table 5 and Table 6, the following conditional formula values can be obtained:

According to Table 5 and Table 6, the following conditional formula values can be obtained:

According to Table 5 and Table 6, the values related to the length of the contour curve can be obtained:

Fourth embodiment

Please refer to FIG. 4A and FIG. 4B, where FIG. 4A is a schematic diagram of an optical imaging system according to a fourth embodiment of the present invention, and FIG. 4B is a diagram of the optical imaging system of the fourth embodiment in order from left to right. Spherical aberration, astigmatism and optical distortion curves. FIG. 4C is a transverse aberration diagram of the meridional fan and the sagittal fan of the optical imaging system of the fourth embodiment at the longest working wavelength and the shortest working wavelength through the aperture edge at a field of view of 0.7. FIG. 4D is a diagram showing the defocus modulation conversion contrast transfer rate of the central field of view, 0.3 field of view, and 0.7 field of view of the visible light spectrum of the fourth embodiment of the present invention; FIG. 4E is a view of the fourth embodiment of the present invention Defocus modulation conversion vs. transfer rate diagram for the central field of view, 0.3 field of view, and 0.7 field of view of the infrared light spectrum. It can be seen from FIG. 4A that the optical imaging system includes a first lens 410, an aperture 400, a second lens 420, a third lens 430, a fourth lens 440, an infrared filter 470, and an imaging surface 480 in order from the object side to the image side. And image sensing element 490.

The first lens 410 has a positive refractive power and is made of plastic. The object side surface 412 is convex, the image side 414 is concave, and both are aspheric. The object side 412 and the image side 414 both have an inflection point.

The second lens 420 has a positive refractive power and is made of a plastic material. Its object side surface 422 is convex, its image side surface 424 is convex, and both are aspheric, and its object side surface 422 has an inflection point.

The third lens 430 has a negative refractive power and is made of plastic. The object side 432 is concave, the image side 434 is convex, and both are aspheric. The object side 432 and the image side 434 each have an inflection point.

The fourth lens 440 has a positive refractive power and is made of plastic. The object side 442 is convex, the image side 444 is concave, and both are aspheric. The object side 442 and the image side 444 both have an inflection point.

The infrared filter 470 is made of glass and is disposed between the fourth lens 440 and the imaging surface 480 without affecting the focal length of the optical imaging system.

In the optical imaging system of the fourth embodiment, the first lens, the second lens, and the fourth lens are all positive lenses, and their individual focal lengths are f1, f2, and f4, and the sum of the focal lengths of all lenses with positive refractive power is ΣPP. It satisfies the following conditions: ΣPP = f1 + f2 + f4. This helps to properly distribute the positive refractive power of a single lens to other positive lenses, so as to suppress the occurrence of significant aberrations during the traveling of incident light.

In the optical imaging system of the fourth embodiment, the individual focal length of the third lens is f3, and the sum of the focal lengths of all lenses with negative refractive power is ΣNP, which satisfies the following conditions: ΣNP = f3.

Please refer to Table 7 and Table 8 below.

In the fourth embodiment, the curve equation of the aspherical surface is expressed as the first embodiment. In addition, the definitions of the parameters in the following table are the same as those in the first embodiment, and will not be repeated here.

According to Table 7 and Table 8, the following conditional formula values can be obtained:

According to Table 7 and Table 8, the following conditional formula values can be obtained:

According to Table 7 and Table 8, the values related to the length of the contour curve can be obtained:

Fifth Embodiment

Please refer to FIG. 5A and FIG. 5B, wherein FIG. 5A shows a schematic diagram of an optical imaging system according to a fifth embodiment of the present invention, and FIG. 5B shows the optical imaging system of the fifth embodiment in order from left to right. Spherical aberration, astigmatism and optical distortion curves. FIG. 5C is a transverse aberration diagram of the meridional fan and the sagittal fan of the optical imaging system according to the fifth embodiment at the longest working wavelength and the shortest working wavelength through the aperture edge at a field of view of 0.7. FIG. 5D is a diagram showing the defocus modulation conversion contrast transfer rate of the central field of view, 0.3 field of view, and 0.7 field of view of the fifth embodiment of the present invention; and FIG. 5E is a view of the fifth embodiment of the present invention. Defocus modulation conversion vs. transfer rate diagram for the central field of view, 0.3 field of view, and 0.7 field of view of the infrared light spectrum. As can be seen from FIG. 5A, the optical imaging system includes a first lens 510, an aperture 500, a second lens 520, a third lens 530, a fourth lens 540, an infrared filter 570, and an imaging surface 580 in order from the object side to the image side. And image sensing element 590.

The first lens 510 has a positive refractive power and is made of plastic. The object side 512 is convex, the image side 514 is concave, and both are aspheric. The object side 512 and the image side 514 both have an inflection point.

The second lens 520 has a positive refractive power and is made of plastic. Its object side 522 is convex, its image side 524 is convex, and both are aspheric. Curving point.

The third lens 530 has a positive refractive power and is made of plastic. The object side 532 is concave, the image side 534 is convex, and both are aspheric. The object side 532 and the image side 534 each have an inflection point.

The fourth lens 540 has a negative refractive power and is made of plastic. Its object side surface 542 is convex, its image side surface 544 is concave, and both are aspheric, and its object side surface 542 and image side surface 544 each have an inflection point.

The infrared filter 570 is made of glass and is disposed between the fourth lens 540 and the imaging surface 580 without affecting the focal length of the optical imaging system.

In the optical imaging system of the fifth embodiment, the first lens, the second lens, and the third lens are all positive lenses, and their individual focal lengths are f1, f2, and f3, and the sum of the focal lengths of all lenses with positive refractive power is ΣPP. It satisfies the following conditions: ΣPP = f1 + f2 + f3. This helps to properly distribute the positive refractive power of a single lens to other positive lenses, so as to suppress the occurrence of significant aberrations during the traveling of incident light.

In the optical imaging system of the fifth embodiment, the sum of the focal lengths of all the lenses with negative refractive power is ΣNP, which satisfies the following conditions: ΣNP = f4.

Please refer to Tables 9 and 10 below.

In the fifth embodiment, the aspherical curve equation is expressed as in the first embodiment. form. In addition, the definitions of the parameters in the following table are the same as those in the first embodiment, and will not be repeated here.

According to Table 9 and Table 10, the following conditional formula values can be obtained:

According to Table 9 and Table 10, the following conditional formula values can be obtained:

According to Table 9 and Table 10, the values related to the length of the contour curve can be obtained:

Sixth embodiment

Please refer to FIG. 6A and FIG. 6B, wherein FIG. 6A shows a schematic diagram of an optical imaging system according to a sixth embodiment of the present invention, and FIG. 6B shows the optical imaging system of the sixth embodiment in order from left to right. Spherical aberration, astigmatism and optical distortion curves. FIG. 6C is a transverse aberration diagram of the meridional fan and the sagittal fan of the optical imaging system according to the sixth embodiment, with the longest working wavelength and the shortest working wavelength passing through the aperture edge at a field of view of 0.7. FIG. 6D is a diagram showing the defocus modulation conversion contrast transfer rate of the central field of view, 0.3 field of view, and 0.7 field of view of the visible light spectrum of the sixth embodiment of the present invention; FIG. 6E is a view of the sixth embodiment of the present invention Defocus modulation conversion vs. transfer rate diagram for the central field of view, 0.3 field of view, and 0.7 field of view of the infrared light spectrum. It can be seen from FIG. 6A that the optical imaging system includes a first lens 610, an aperture 600, a second lens 620, a third lens 630, a fourth lens 640, an infrared filter 670, and an imaging surface 680 in order from the object side to the image side. And an image sensing element 690.

The first lens 610 has a positive refractive power and is made of a plastic material. Its object side 612 is convex, its image side 614 is concave, and both are aspheric. The object side 612 has an inflection point.

The second lens 620 has a positive refractive power and is made of plastic. Its object side 622 is convex, its image side 624 is convex, and both are aspheric, and its object side 622 has an inflection point.

The third lens 630 has a positive refractive power and is made of plastic. Its object side 632 is concave, its image side 634 is convex, and all of them are aspheric, and its object side 632 has an inflection point.

The fourth lens 640 has a negative refractive power and is made of plastic. The object side 642 is convex, the image side 644 is concave, and both are aspheric. The object side 642 and the image side 644 both have an inflection point.

The infrared filter 670 is made of glass and is disposed between the fourth lens 640 and the imaging surface 680 without affecting the focal length of the optical imaging system.

In the optical imaging system of the fifth embodiment, the first lens, the second lens, and the third lens are all positive lenses, and their individual focal lengths are f1, f2, and f3, and the total focal length of all lenses with positive refractive power is ΣPP. It satisfies the following conditions: ΣPP = f1 + f2 + f3. This helps to properly distribute the positive refractive power of a single lens to other positive lenses, so as to suppress the occurrence of significant aberrations during the traveling of incident light.

In the optical imaging system of the fifth embodiment, the sum of the focal lengths of all the lenses with negative refractive power is ΣNP, which satisfies the following conditions: ΣNP = f4.

Please refer to Table 11 and Table 12 below.

In the sixth embodiment, the curve equation of the aspherical surface is expressed as the first embodiment. In addition, the definitions of the parameters in the following table are the same as those in the first embodiment, and will not be repeated here.

According to Table 11 and Table 12, the following conditional formula values can be obtained:

According to Table 11 and Table 12, the following conditional formula values can be obtained:

According to Table 11 and Table 12, the relevant values of the contour curve length can be obtained:

Although the present invention has been disclosed in the above embodiments, it is not intended to limit the present invention. Any person skilled in the art can make various modifications and retouches without departing from the spirit and scope of the present invention. Therefore, the protection of the present invention The scope shall be determined by the scope of the attached patent application.

Although the invention has been particularly shown and described with reference to exemplary embodiments thereof, It will be understood by those having ordinary knowledge in the technical field that various changes in form and details can be made thereto without departing from the spirit and scope of the invention as defined by the following patent application scope and equivalents thereof.

Claims (22)

An optical imaging system includes: a first lens having a refractive power; a second lens having a refractive power; a third lens having a refractive power; a fourth lens having a refractive power A first imaging plane; it is a visible light image plane perpendicular to the optical axis and its central field of view has a maximum defocus modulation conversion contrast transfer rate (MTF) at a first spatial frequency; and a second imaging Plane; it is a specific infrared light image plane perpendicular to the optical axis and its center field of view has a maximum defocus modulation conversion contrast transfer rate (MTF) at the first spatial frequency, where the optical imaging system has a refractive power There are four lenses. At least one of the first lens to the fourth lens has a positive refractive power. The focal lengths of the first lens to the fourth lens are f1, f2, f3, and f4, respectively. The focal length of the optical imaging system. Is f, the entrance pupil diameter of the optical imaging system is HEP, the distance from the object side of the first lens to the first imaging plane is HOS on the optical axis, and the distance from the object side of the first lens to the image side of the fourth lens is on the light A distance on the axis From InTL, half of the maximum viewing angle of the optical imaging system is HAF. The optical imaging system has a maximum imaging height HOI perpendicular to the optical axis on the first imaging plane, between the first imaging plane and the second imaging plane. The distance on the optical axis is FS, the wavelength of the infrared light is between 700nm and 1000nm, and the first spatial frequency is represented by SP1. The intersection of any surface of any of the lenses and the optical axis is the starting point and extends The contour of the surface is up to the coordinate point on the surface at a vertical height of 1/2 of the entrance pupil diameter from the optical axis. The length of the contour curve between the two points is ARE; it satisfies the following conditions: 1 ≦ f / HEP ≦ 10; 0deg <HAF ≦ 70deg; SP1 ≦ 440 cycles / mm; 1 ≦ 2 (ARE / HEP) ≦ 2.0; and | FS | ≦ 30 μm. The optical imaging system according to claim 1, wherein the image side of the second lens and the image side of the third lens are convex on the optical axis. The optical imaging system according to claim 1, wherein half of the maximum vertical viewing angle of the optical imaging system is VHAF, and the optical imaging system satisfies the following formula: VHAF ≧ 10deg. The optical imaging system according to claim 1, wherein the optical imaging system satisfies the following conditions: HOS / HOI ≧ 1.2. The optical imaging system according to claim 1, wherein the intersection of the object-side surface of the fourth lens on the optical axis is a starting point, and the contour of the surface is extended until the surface is perpendicular to 1/2 the entrance pupil diameter of the optical axis Up to the coordinate point at the height, the length of the contour curve between the two points is ARE41, the intersection of the image-side surface of the fourth lens on the optical axis is the starting point, and the contour of the surface is extended until the surface is 1/0 from the optical axis. 2 Up to the coordinate point at the vertical height of the entrance pupil diameter, the length of the contour curve between the two points is ARE42, and the thickness of the fourth lens on the optical axis is TP4, which satisfies the following conditions: 0.05 ≦ ARE41 / TP4 ≦ 25; and 0.05 ≦ ARE42 / TP4 ≦ 25. The optical imaging system according to claim 1, wherein the first lens has a negative refractive power. The TV distortion of the optical imaging system at the time of image formation is TDT, and the longest working wavelength of the positive meridional fan of the optical imaging system passes through the edge of the entrance pupil and enters the lateral aberration at 0.7HOI on the imaging plane. PLTA indicates that the shortest working wavelength of the positive meridional fan passes through the edge of the entrance pupil and is incident on the imaging surface at 0.7HOI. The lateral aberration is represented by PSTA, and the longest working wavelength of the negative meridional fan passes through the incident. The lateral aberration of the pupil edge and incident on the imaging plane at 0.7HOI is represented by NLTA. The shortest working wavelength of the negative meridional fan passes through the entrance pupil edge and is incident on the imaging plane at 0.7HOI. NSTA indicates that the longest working wavelength of the sagittal plane fan passes through the edge of the entrance pupil and is incident on the imaging plane at 0.7HOI. The lateral aberration is represented by SLTA. The lateral aberration at 0.7HOI on the imaging surface is represented by SSTA, which satisfies the following conditions: PLTA ≦ 100 μm; PSTA ≦ 100 μm; NLTA ≦ 100 μm; NSTA ≦ 100 μm; SLTA ≦ 100 μm; and SST A ≦ 100 microns; | TDT | <100%. The optical imaging system according to claim 1, further comprising an aperture, and a distance InS on the optical axis from the aperture to the first imaging plane, which satisfies the following formula: 0.2 ≦ InS / HOS ≦ 1.1. An optical imaging system includes, in order from the object side to the image side, a first lens having a positive refractive power, a second lens having a refractive power, and an image side thereof is convex on an optical axis; and a third lens having a Inflection force, whose image side is convex on the optical axis; a fourth lens with inflection force; a first imaging surface; it is a visible light image plane perpendicular to the optical axis and its central field of view is in the first space Frequency (220cycles / mm) has a maximum out-of-focus modulation conversion contrast transfer rate (MTF); and a second imaging plane; it is a specific infrared light image plane perpendicular to the optical axis and its central field of view is first The defocus modulation conversion contrast transfer rate (MTF) of the spatial frequency (220cycles / mm) has a maximum value, wherein the optical imaging system has four lenses having a refractive power, and at least one of the second lens to the fourth lens has Positive refractive power, the focal lengths of the first lens to the fourth lens are f1, f2, f3, f4, the focal length of the optical imaging system is f, the entrance pupil diameter of the optical imaging system is HEP, and the first lens object Side to the first imaging plane at There is a distance HOS on the axis, the object side of the first lens to the image side of the fourth lens has a distance InTL on the optical axis, half of the maximum viewing angle of the optical imaging system is HAF, and the optical imaging system is on the first The imaging plane has a maximum imaging height HOI perpendicular to the optical axis. The intersection point of any surface of any of these lenses with the optical axis is the starting point, and extends the contour of the surface until the surface is 1/2 incident from the optical axis. Up to the coordinate point at the vertical height of the pupil diameter, the length of the contour curve between the two points is ARE, and the distance between the first imaging plane and the second imaging plane is FS; it satisfies the following conditions: 1 ≦ f / HEP ≦ 10; 0deg <HAF ≦ 70deg; | FS | ≦ 30 μm and 1 ≦ 2 (ARE / HEP) ≦ 2.0. The optical imaging system according to claim 8, wherein the maximum effective radius of any surface of any of the lenses is represented by EHD, and the intersection point of any surface of any of the lenses with the optical axis is used as a starting point, Extend the contour of the surface until the maximum effective radius of the surface is the end point. The length of the contour curve between the two points is ARS, which satisfies the following formula: 1 ≦ ARS / EHD ≦ 2.0. The optical imaging system according to claim 8, wherein half of the maximum vertical viewing angle of the optical imaging system is VHAF, and the optical imaging system satisfies the following formula: VHAF ≧ 20deg. The optical imaging system according to claim 8, wherein the optical imaging system satisfies the following conditions: HOS / HOI ≧ 1.4. The optical imaging system according to claim 8, wherein the third lens has a positive refractive power. The optical imaging system according to claim 8, wherein the fourth lens has a negative refractive power, and the image side of the second lens and the image side of the third lens are convex on the optical axis. The optical imaging system according to claim 8, wherein a distance on the optical axis between the third lens and the fourth lens is IN34, and satisfies the following formula: 0 <IN34 / f ≦ 5. The optical imaging system according to claim 8, wherein a distance on the optical axis between the first lens and the second lens is IN12, and satisfies the following formula: 0 <IN12 / f ≦ 60. The optical imaging system according to claim 8, wherein the distance between the third lens and the fourth lens on the optical axis is IN34, and the thicknesses of the third lens and the fourth lens on the optical axis are TP3 and TP4, which satisfies the following conditions: 1 ≦ (TP4 + IN34) / TP3 ≦ 10. The optical imaging system according to claim 8, wherein at least one surface of each of at least one of the first lens to the fourth lens has at least one inflection point. An optical imaging system includes, in order from the object side to the image side, a first lens having a positive refractive power, a second lens having a refractive power, and an image side thereof is convex on an optical axis; and a third lens having a Inflection force, the image side of which is convex on the optical axis; a fourth lens with inflection force; a first average imaging surface; it is a visible light image plane perpendicular to the optical axis and is arranged on the optical imaging system The central field of view, the field of view of 0.3, and the field of view of 0.7 each have the average position of the out-of-focus position at the first spatial frequency (220 cycles / mm) of each of the maximum MTF values of the field of view; and a second average imaging plane; It is a specific infrared light image plane perpendicular to the optical axis and is set at the central field of view, 0.3 field of view and 0.7 field of view of the optical imaging system. Each of the first spatial frequencies (220 cycles / mm) has a maximum MTF of the field of view. The average position of the defocus position of the value, wherein the optical imaging system has four lenses having a refractive power, at least one of the third lens to the fourth lens has a positive refractive power, and the first lens to the fourth lens The focal lengths are f1, f2, f3, f4, the focal length of the optical imaging system is f, the entrance pupil diameter of the optical imaging system is HEP, the object lens side to the first imaging plane has a distance HOS on the optical axis, the There is a distance InTL on the optical axis from the object side of the first lens to the image side of the fourth lens. Half of the maximum viewing angle of the optical imaging system is HAF. The optical imaging system is perpendicular to the optical axis on the first average imaging plane. It has a maximum imaging height HOI. The intersection of any surface of any of these lenses with the optical axis is the starting point, and extends the contour of the surface until the vertical height of the surface is 1/2 of the entrance pupil diameter from the optical axis. Up to the coordinate point, the length of the contour curve between the two points is ARE, the distance between the first average imaging surface and the second average imaging surface is AFS; half of the maximum vertical viewing angle of the optical imaging system is VHAF, which satisfies The following conditions: 1 ≦ f / HEP ≦ 10; 0deg <HAF ≦ 70deg; | AFS | ≦ 30μm; VHAF ≧ 20deg and 1 ≦ 2 (ARE / HEP) ≦ 2.0. The optical imaging system according to claim 18, wherein the maximum effective radius of any surface of any of the lenses is represented by EHD, and the intersection of any surface of any of the lenses with the optical axis is the starting point, Extend the contour of the surface until the maximum effective radius of the surface is the end point. The length of the contour curve between the two points is ARS, which satisfies the following formula: 1 ≦ ARS / EHD ≦ 2.0. The optical imaging system according to claim 18, wherein the optical imaging system satisfies the following conditions: HOS / HOI ≧ 1.6. The optical imaging system according to claim 18, wherein the optical imaging system further includes an aperture and an image sensing element, the image sensing element is disposed behind the first average imaging surface and is provided with at least 100,000 pixels, and There is a distance InS on the optical axis from the aperture to the first average imaging plane, which satisfies the following formula: 0.2 ≦ InS / HOS ≦ 1.1. The optical imaging system according to claim 18, wherein the optical imaging system further includes an aperture, an image sensing element, and a driving module. The image sensing element is disposed behind the first imaging surface and at least 100,000. Pixels, and a distance InS on the optical axis from the aperture to the first average imaging plane, the driving module can be coupled to the lenses and cause the lenses to be displaced, which satisfies the following formula: 0.2 ≦ InS /HOS≦1.1.